INTELSAT 33E DEB, 61990

Orbit data source: Space-Track

INTELSAT 33E DEB, 61990 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.

Not visible in the next 10 days

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Identifier	61990, 2016-053G
Orbit	GEO
Last TLE update	1 week 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 week ago

0 INTELSAT 33E DEB
1 61990U 16053G   25082.62000381 -.00000221  00000-0  00000-0 0  9993
2 61990   0.3610  55.2506 0172287 306.8025 358.0069  1.01377199  1584

Epoch: 2025-03-23T14:52Z

Definitive object data (Epoch: 2025-03-23T14:52:48.329Z)

Latitude	-0.29808°
Longitude	-44.54909°
Altitude	34,755.428 km
Speed	3.14 km/s
True Right ascension	00h 00m 00s
True Declination	0° 17' 52"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	0.34699°
Longitude	116.41535°
Altitude	36,152.459 km
Speed	3.037 km/s
Apparent Right ascension	11h 09m 49s
Apparent Declination	-5° 02' 45"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	04:25:54
Azimuth	86.822° E
Elevation	-11.652°
Doppler factor	1

Orbital elements

Apogee altitude	36,201.777 km
Perigee altitude	34,759.433 km
Semi-major axis	41,858.742 km
Eccentricity	0.0172287
Inclination	0.361°
RAAN	55.2506°
Arg. of periapsis	306.8025°
True anomaly	357.93673°
Mean anomaly	358.0069°
Eccentric anomaly	357.97197°
Mean motion	0.25343 °/min
BSTAR	Unknown
Orbital period	1420.49 mins