CTS DEB (ARRAY COVER), 39689

Orbit data source: Space-Track

CTS DEB (ARRAY COVER), 39689 is space debris in GEO originally from a launch on Sat, 17 Jan 1976 UTC launched from the Air Force Eastern Test Range (AFETR). 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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CTS DEB (ARRAY COVER) details

Identifier	39689, 1976-004F
Orbit	GEO
Last TLE update	4 days ago
Origin	CRC (CA)
Manufacturer	CRC
Mission	Spacecraft
Bus & Motor	Unknown
Mass	Wet unknown, 4 kg dry
Launch date (UTC)	1976-01-17 (49 years ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 1.8 m
Radar Cross Section	1.800 m²

Expand to show TLE details & history

TLE from 4 days ago

0 CTS DEB (ARRAY COVER)
1 39689U 76004F   24357.87445621  .00000035  00000-0  00000-0 0  9998
2 39689   4.6664 275.8491 0160176  40.0641 321.3207  1.00273773 61460

Epoch: 2024-12-22T20:59Z

Definitive object data (Epoch: 2024-12-22T20:59:13.016Z)

Latitude	0°
Longitude	-130.64481°
Altitude	35,261.19 km
Speed	3.113 km/s
True Right ascension	18h 24m 15s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-4.26984°
Longitude	163.26798°
Altitude	35,959.733 km
Speed	3.062 km/s
Apparent Right ascension	13h 46m 53s
Apparent Declination	-10° 47' 28"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	15:44:04
Azimuth	214.732° SW
Elevation	32.475°
Doppler factor	1

Orbital elements

Apogee altitude	36,462.484 km
Perigee altitude	35,111.712 km
Semi-major axis	42,165.235 km
Eccentricity	0.0160176
Inclination	4.6664°
RAAN	275.8491°
Arg. of periapsis	40.0641°
True anomaly	320.15547°
Mean anomaly	321.3207°
Eccentric anomaly	320.73992°
Mean motion	0.25068 °/min
BSTAR	Unknown
Orbital period	1436.12 mins