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

INTELSAT 33E DEB details

Identifier	61992, 2016-053J
Orbit	GEO
Last TLE update	4 days ago
Origin	Intelsat SA (US) (US / ITSO)
Manufacturer	Boeing/ES
Mission	Spacecraft
Bus & Motor	Unknown
Mass	Unknown
Launch date (UTC)	2016-08-24 (8 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 4 days ago

0 INTELSAT 33E DEB
1 61992U 16053J   24324.50291974 -.00000319  00000-0  00000-0 0  9998
2 61992   0.0817 108.2045 0046381 227.1808  24.4136  1.00794627   315

Epoch: 2024-11-19T12:04Z

Definitive object data (Epoch: 2024-11-19T12:04:12.265Z)

Latitude	-0.06004°
Longitude	119.93642°
Altitude	35,463.54 km
Speed	3.093 km/s
True Right ascension	23h 59m 59s
True Declination	0° 03' 36"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-0.07354°
Longitude	141.24431°
Altitude	35,504.921 km
Speed	3.09 km/s
Apparent Right ascension	01h 05m 20s
Apparent Declination	-5° 14' 06"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	09:54:06
Azimuth	295.957° NW
Elevation	-34.856°
Doppler factor	1

Orbital elements

Apogee altitude	35,836.624 km
Perigee altitude	35,446.839 km
Semi-major axis	42,019.868 km
Eccentricity	0.0046381
Inclination	0.0817°
RAAN	108.2045°
Arg. of periapsis	227.1808°
True anomaly	24.63444°
Mean anomaly	24.4136°
Eccentric anomaly	24.5239°
Mean motion	0.25198 °/min
BSTAR	Unknown
Orbital period	1428.7 mins