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.

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Identifier
61992, 2016-053J
Orbit
GEO
Country
Flag of USUS / ITSO
Related business
Manufacturer
Boeing/ES
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Icon of a cake. It is the launch day of the satellite!2016-08-24 (10 years ago)
Launch vehicle
Unknown
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 INTELSAT 33E DEB
1 61992U 16053J   26234.60800885 -.00000155  00000-0  00000-0 0  9996
2 61992   1.7268  82.8987 0046385 324.7915  35.2000  1.00808257  6784
Epoch: 2026-08-22T14:35Z
TLE epoch observation values (Epoch: 2026-08-22T14:35:31.964Z)
Latitude
0.00001°
Longitude
-106.5984°
Altitude
35,478.204 km
Speed
3.092 km/s
True Right ascension
05h 32m 48s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
16:02:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,832.834 km
Perigee altitude
35,443.051 km
Semi-major axis
42,016.079 km
Eccentricity
0.00464
Inclination
1.7268°
RAAN
82.8987°
Arg. of periapsis
324.7915°
True anomaly
35.50785°
Mean anomaly
35.2°
Eccentric anomaly
35.35378°
Mean motion
0.25201 °/min
Orbital period
1,428.51 mins
BSTAR
0
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