GHGSAT-D, 41602 (Decayed)

Orbit data source: Space-Track

GHGSAT-D, 41602 was a Canadian payload satellite in LEO that was launched on Wed, 22 Jun 2016 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Not visible in the next 10 days

GHGSAT-D details

Identifier	41602, 2016-040D
Orbit	Decayed
Last TLE update	2 weeks ago
Origin	GHG/UTIAS (CA)
Manufacturer	UTIAS-SFL
Mission	Decayed Amateur Science
Bus & Motor	NEMO-V1, Unknown motor
Mass	25 kg wet, 25 kg dry
Launch date (UTC)	2016-06-22 (9 years ago)
Launch vehicle	PSLV-XL
Launch site	Sirharikota (SRI)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 0.4 m
Radar Cross Section	0.160 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 2 weeks ago

0 GHGSAT-D
1 41602U 16040D   24344.00039522  .17095095  22406-5  17075-3 0  9990
2 41602  97.0378  26.0013 0005524 297.6473  62.4272 16.51130145472525

Epoch: 2024-12-09T00:00Z

Definitive object data (Epoch: 2024-12-09T00:00:34.146Z)

Latitude	-0.00008°
Longitude	-52.37103°
Altitude	137.973 km
Speed	7.824 km/s
True Right ascension	01h 44m 00s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	136.735 km
Perigee altitude	129.542 km
Semi-major axis	6,511.275 km
Eccentricity	0.0005524
Inclination	97.0378°
RAAN	26.0013°
Arg. of periapsis	297.6473°
True anomaly	62.48333°
Mean anomaly	62.4272°
Eccentric anomaly	62.45526°
Mean motion	4.13089 °/min
BSTAR	0.00017075
Orbital period	87.15 mins