INTELSAT 33E DEB, 61996

Orbit data source: Space-Track

INTELSAT 33E DEB, 61996 is space debris in GEO originally from a launch on Wed, 24 Aug 2016 UTC launched from the French Guiana (FRGUI). 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.

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Identifier	61996, 2016-053N
Orbit	GEO
Last TLE update	1 month ago
Origin	INTEL (US / ITSO)
Manufacturer	Boeing/ES
Mission	Spacecraft
Bus & Motor	Unknown
Mass	Unknown
Launch date (UTC)	2016-08-24 (9 years ago)
Launch vehicle	Unknown
Launch site	French Guiana (FRGUI)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	RCS unknown

Expand to show TLE details & history

TLE from 1 month ago

0 INTELSAT 33E DEB
1 61996U 16053N   25046.03797800  .00000131  00000-0  00000-0 0  9992
2 61996   0.4069  18.7924 0054117   0.9516 340.4290  1.00601379  1204

Epoch: 2025-02-15T00:54Z

Definitive object data (Epoch: 2025-02-15T00:54:41.299Z)

Latitude	-0.15172°
Longitude	-158.96269°
Altitude	35,479.37 km
Speed	3.094 km/s
True Right ascension	00h 00m 00s
True Declination	0° 09' 06"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	0.33415°
Longitude	-88.45259°
Altitude	35,541.982 km
Speed	3.089 km/s
Apparent Right ascension	04h 42m 49s
Apparent Declination	-5° 54' 04"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	04:36:04
Azimuth	177.656° S
Elevation	44.156°
Doppler factor	1

Orbital elements

Apogee altitude	35,923.213 km
Perigee altitude	35,467.833 km
Semi-major axis	42,073.66 km
Eccentricity	0.0054117
Inclination	0.4069°
RAAN	18.7924°
Arg. of periapsis	0.9516°
True anomaly	340.21994°
Mean anomaly	340.429°
Eccentric anomaly	340.3246°
Mean motion	0.25149 °/min
BSTAR	Unknown
Orbital period	1431.45 mins