DECAYED

GSLV R/B, 56082 (Decayed)

Orbit data source: Space-Track

GSLV R/B, 56082 was space debris in LEO originally from an Indian launch on Sun, 26 Mar 2023 UTC launched from the Sirharikota (SRI). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

Not visible in the next 10 days

GSLV R/B details

Identifier	56082, 2023-043AN
Orbit	Decayed
Last TLE update	7 months ago
Origin	NSIL/ISRO (IN / IND)
Manufacturer	ISRO
Mission	Decayed spacecraft
Bus & Motor	C25, CE-20
Mass	4,400 kg wet, 4,400 kg dry
Launch date (UTC)	2023-03-26 (2 years ago)
Launch vehicle	Unknown
Launch site	Sirharikota (SRI)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl + 1 Nozzle, 13.545 m
Radar Cross Section	48.836 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 7 months ago

0 GSLV R/B
1 56082U 23043AN  24166.54356647  .24880644 -14000-5  14634-3 0  9990
2 56082  87.3709 340.3933 0012142 257.4446 216.5646 16.54439776 69393

Epoch: 2024-06-14T13:02Z

Definitive object data (Epoch: 2024-06-14T13:02:44.143Z)

Latitude	66.03019°
Longitude	55.49532°
Altitude	145.574 km
Speed	7.821 km/s
True Right ascension	10h 17m 59s
True Declination	65° 53' 25"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	36.52311°
Longitude	178.79968°
Altitude	139.315 km
Speed	8.748 km/s
Apparent Right ascension	22h 44m 17s
Apparent Declination	-3° 12' 39"
Sunlit	Object is in full shadow

Visualization observer readout

Local Sidereal Time	15:36:03
Azimuth	81.364° E
Elevation	-15.104°
Doppler factor	1

Orbital elements

Apogee altitude	132.207 km
Perigee altitude	116.417 km
Semi-major axis	6,502.449 km
Eccentricity	0.0012142
Inclination	87.3709°
RAAN	340.3933°
Arg. of periapsis	257.4446°
True anomaly	216.48181°
Mean anomaly	216.5646°
Eccentric anomaly	216.5232°
Mean motion	4.13931 °/min
BSTAR	0.00014634
Orbital period	86.97 mins