INTELSAT 33E DEB, 61992

Orbit data source: Space-Track

INTELSAT 33E DEB, 61992 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	61992, 2016-053J
Orbit	GEO
Last TLE update	1 day 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 day ago

0 INTELSAT 33E DEB
1 61992U 16053J   25089.45977056  .00000108  00000-0  00000-0 0  9998
2 61992   0.4183  91.7204 0056438 278.2301 350.1554  1.00791342  1648

Epoch: 2025-03-30T11:02Z

Definitive object data (Epoch: 2025-03-30T11:02:04.176Z)

Latitude	-0.40859°
Longitude	6.39267°
Altitude	35,406.251 km
Speed	3.097 km/s
True Right ascension	23h 59m 59s
True Declination	0° 24' 29"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	0.41087°
Longitude	-172.99125°
Altitude	35,875.973 km
Speed	3.063 km/s
Apparent Right ascension	12h 25m 27s
Apparent Declination	-4° 50' 21"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	04:24:23
Azimuth	73.34° E
Elevation	-26.06°
Doppler factor	1

Orbital elements

Apogee altitude	35,879.801 km
Perigee altitude	35,405.487 km
Semi-major axis	42,020.781 km
Eccentricity	0.0056438
Inclination	0.4183°
RAAN	91.7204°
Arg. of periapsis	278.2301°
True anomaly	350.04405°
Mean anomaly	350.1554°
Eccentric anomaly	350.0998°
Mean motion	0.25197 °/min
BSTAR	Unknown
Orbital period	1428.75 mins