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OPS 9326 (IDSCS 13), 2653

Orbit data source: Space-Track

OPS 9326 (IDSCS 13), 2653 is a payload satellite owned by USAF SSD (US) in GEO that was launched on Wed, 18 Jan 1967 UTC via a TITAN IIIC launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets 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.

Not visible in the next 10 days

OPS 9326 (IDSCS 13) details

Identifier	2653, 1967-003F
Orbit	GEO
Last TLE update	1 week ago
Origin	USAF SSD (US)
Manufacturer	Philco-Ford WDL
Mission	Non-operational Defense Communications
Bus & Motor	IDCSP, Unknown motor
Mass	45 kg wet, 45 kg dry
Launch date (UTC)	1967-01-18 (58 years ago)
Launch vehicle	TITAN IIIC
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Ico Poly, 0.9 m
Radar Cross Section	0.926 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 1 week ago

0 OPS 9326 (IDSCS 13)
1  2653U 67003F   25015.26246088 -.00000084  00000-0  00000+0 0  9993
2  2653   7.1900  50.8165 0044732  50.0399 310.3851  1.07748732127141

Epoch: 2025-01-15T06:17Z

Definitive object data (Epoch: 2025-01-15T06:17:56.62Z)

Latitude	0.00001°
Longitude	-158.57505°
Altitude	33,695.938 km
Speed	3.158 km/s
True Right ascension	03h 23m 28s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	3.90937°
Longitude	-126.04416°
Altitude	33,639.544 km
Speed	3.163 km/s
Apparent Right ascension	05h 36m 21s
Apparent Declination	-1° 43' 13"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	17:58:54
Azimuth	9.07° NNE
Elevation	-51.462°
Doppler factor	1

Orbital elements

Apogee altitude	33,993.582 km
Perigee altitude	33,634.009 km
Semi-major axis	40,191.933 km
Eccentricity	0.0044732
Inclination	7.19°
RAAN	50.8165°
Arg. of periapsis	50.0399°
True anomaly	309.99324°
Mean anomaly	310.3851°
Eccentric anomaly	310.18931°
Mean motion	0.26936 °/min
BSTAR	Unknown
Orbital period	1336.5 mins