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CTS, 8585

Orbit data source: Space-Track

CTS, 8585 is a payload satellite owned by CRC (CA) in GEO that was launched on Sat, 17 Jan 1976 UTC via a DELTA 2914 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
8585, 1976-004A
Orbit
GEO
Country
Flag of CACA
Related business
Manufacturer
CRC
Mission
Spacecraft
Bus & Motor
CTS, Unknown motor
Mass
685 kg wet, 311 kg dry
Launch date (UTC)
1976-01-17 (50 years ago)
Launch vehicle
DELTA 2914
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 CTS
1 08585U 76004A   26092.06850337 -.00000098  00000-0  00000-0 0  9992
2 08585   4.1263 273.1285 0010866 284.9359 273.0900  1.00200434121530
Epoch: 2026-04-02T01:38Z
TLE epoch observation values (Epoch: 2026-04-02T01:38:38.691Z)
Latitude
-1.29733°
Longitude
-104.07768°
Altitude
35,803.749 km
Speed
3.074 km/s
True Right ascension
07h 24m 01s
True Declination
-1° 17' 46"
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
02:13:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,853.51 km
Perigee altitude
35,761.832 km
Semi-major axis
42,185.808 km
Eccentricity
0.00109
Inclination
4.1263°
RAAN
273.1285°
Arg. of periapsis
284.9359°
True anomaly
272.96566°
Mean anomaly
273.09°
Eccentric anomaly
273.02783°
Mean motion
0.25049 °/min
Orbital period
1,437.17 mins
BSTAR
0
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