Thursday 8 December 2016

OT: the slow, 13.8 second duration earthgrazing fireball over the Netherlands of 28 Nov 2016, 04:40 UT

the long duration (13.8 s) fireball of 28 Nov 2016, 4:40 UT 
image (c) Jos Nijland, Benningbroek, NL - click to enlarge


In the early morning of 28 November 2016, near 04:40 UT (05:40 am local time), a bright, slow fireball with an extremely long duration occurred over the Netherlands.

The image above was captured by the all sky meteor camera of Jos Nijland in Benningbroek and shows how the fireball trajectory spanned much of the sky. This camera was  equipped with a rotating shutter, and the number of breaks visible in the trail amount to at least 13.8 seconds visibility. That is very long for a fireball.

With such slow, long duration fireballs, one of the first questions asked usually is: is it a meteor, or is it the re-entry of artificial space debris? In this case, the analytical results clearly show it was not an artificial object, but a meteoric fireball of asteroidal origin - i.e. a small chunk of asteroid entering the atmosphere.

A total of 7 all sky photographic cameras captured the fireball: apart from Benningbroek (Jos Nijland) shown above,  it was also captured by stations Ermelo (Koen Miskotte), Oostkapelle (Klaas Jobse), Utrecht (Felix Bettonvil), Bussloo (Jaap van 't Leven), Borne (Peter van Leuteren) and Twisk (Marco Verstraaten). Benningbroek also captured the last few seconds of the fireball on video with a CAMS camera. Koen Miskotte in Ermelo in the center of the Netherlands also observed the fireball visually, estimating it magnitude -5. He reported fragmentation.

Click to enlarge

The photographs allow to reconstruct the atmospheric trajectory, speed, radiant point and heliocentric orbit of this fireball, and whether something survived at the end or not.

The fireball appeared between 04:40:26 and 04:40:40 UT. It entered the atmosphere on a grazing shallow angle of only 11.2 degrees. The trajectory was over 180 km long - the average trajectory for all stations combined is 183 km long, but some stations captured an even longer part, with Benningbroek topping all with 212 km trajectory length! The fireball started over the North Sea at an altitude of 77 km near 53.0 N, 3.1 E (average of all stations), and moved on an almost due West-East trajectory, over the tip of North Holland province and Lake IJssel, ending at 42 km altitude over the northern part of the Noordoost Polder near 52.8 N, 5.7 E.

Four of the 7 stations were equipped with a rotating shutter in front of the lens, allowing speed reconstructions. Combined with the radiant point determination, this yields the orbit in the solar system.

The fireball entered the atmosphere with an initial atmospheric speed of 15.45 km/s. At the end of the trajectory, at 42.3 km altitude, it had slowed down to a terminal speed of 9.3 km/s. At that point, nothing was left of the original meteoroid: no meteorites reached the ground, it had completely ablated away. The deceleration curve obtained is actually quite nice:


Click diagram to enlarge


The apparent radiant of the fireball was low in the western sky, at RA 53.2 degrees, DEC +13.0 degrees in Taurus. The geocentric radiant (the radiant point corrected for amongst others gravitational influence) was at RA 43.8 degrees, DEC +0.4 degrees. The geocentric speed was 11.1 km/s.

Click star map to enlarge

The resulting heliocentric orbit is that of an Apollo asteroid, with perihelion at 0.874 AU, aphelion squarely in the asteroid belt at 2.76 AU, an orbital eccentricity of 0.518 and an orbital inclination of  4.9 degrees.

Click to enlarge


 

Friday 2 December 2016

SIGINT Galore!


USA 136 (Trumpet 3), a TRUMPET in HEO. 28 Nov 2016
click to enlarge

The evening of 28 November was very clear - no moon and an extremely transparent sky, with temperatures around zero.

I used it to target several objects in GEO and HEO. Due to the favourable sky I could use exposure times twice as long as usual.

All the classified objects imaged were Signals Intelligence (SIGINT) satellites, i.e. eavesdropping satellites. The image above shows you one of the TRUMPET satellites, USA 136 (1997-068A), crossing through Andromeda. This is an object in a 63 degree inclined HEO orbit. The satellite was coming down from apogee at that moment and at an altitude of ~31 500 km.

Below is another object in HEO, USA 184 (2006-027A). This too is a SIGINT satellite, part of the TRUMPET-Follow On program (aka Advanced TRUMPET. It also serves as a SBIRS platform.

USA 184, a TRUMPET-FO in HEO, 28 Nov 2016
click to enlarge

This object was near apogee at this moment, at an altitude of 39 000 km over the Faroƫr Islands, which is why it looks stellar in this 20-second exposure. The star field is in Cassiopeia.

Both these objects hadn't been observed by our network for a while, hence they were somewhat off their predictions (1.5 degrees in position in the case of USA 136; and 1 degree off position in the case of USA 184).

I also briefly imaged a part of the geosynchronous belt, much lower in the sky. The targetted GEO objects were SIGINT satellites too: both Mercury 1 and Mercury 2 (1994-054A and 1996-026A), The Advanced ORION satellites Mentor 4 and Mentor 6 (2009-001A and 2012-034A) and the NEMESIS satellite PAN (2009-047A).

PAN and Mentor 4 (both shown below) have a story attached to them and were the subject of my recent article in The Space Review, which you can read here.

PAN (USA 207), a NEMESIS in GEO, 28 Nov 2016
click to enlarge

Mentor 4 (USA 202), an Advanced ORION in GEO, 28 Nov 2016
click to enlarge