INTELSAT 29E DEB, 62723

Orbit data source: Space-Track

INTELSAT 29E DEB, 62723 is space debris in GEO originally from a launch on Wed, 27 Jan 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 29E DEB details

Identifier	62723, 2016-004E
Orbit	GEO
Last TLE update	2 weeks ago
Origin	Arianespace (US / ITSO)
Manufacturer	Unknown
Mission	Spacecraft
Bus & Motor	Unknown
Mass	Unknown
Launch date (UTC)	2016-01-27 (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 2 weeks ago

0 INTELSAT 29E DEB
1 62723U 16004E   25020.88965250 -.00000067  00000-0  00000-0 0  9997
2 62723   5.2395  76.6590 0366036 304.2142  52.3626  1.00540857  1363

Epoch: 2025-01-20T21:21Z

Definitive object data (Epoch: 2025-01-20T21:21:05.975Z)

Latitude	-0°
Longitude	-4.12104°
Altitude	34,812.426 km
Speed	3.144 km/s
True Right ascension	05h 06m 37s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-1.61353°
Longitude	-21.90466°
Altitude	34,475.088 km
Speed	3.169 km/s
Apparent Right ascension	04h 18m 58s
Apparent Declination	-6° 53' 34"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	20:13:02
Azimuth	74.132° E
Elevation	-28.339°
Doppler factor	1

Orbital elements

Apogee altitude	37,253.059 km
Perigee altitude	34,171.729 km
Semi-major axis	42,090.531 km
Eccentricity	0.0366036
Inclination	5.2395°
RAAN	76.659°
Arg. of periapsis	304.2142°
True anomaly	55.77749°
Mean anomaly	52.3626°
Eccentric anomaly	54.0606°
Mean motion	0.25134 °/min
BSTAR	Unknown
Orbital period	1432.31 mins