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OPS 9327 (IDSCS 14), 2654

Orbit data source: Space-Track

OPS 9327 (IDSCS 14), 2654 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 9327 (IDSCS 14) details

Identifier	2654, 1967-003G
Orbit	GEO
Last TLE update	22 hours 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 22 hours ago

0 OPS 9327 (IDSCS 14)
1 02654U 67003G   24355.62141821 -.00000092  00000-0  00000-0 0  9999
2 02654   7.0997  51.9157 0056585  35.8110 340.5354  1.07511217133631

Epoch: 2024-12-20T14:54Z

Definitive object data (Epoch: 2024-12-20T14:54:50.533Z)

Latitude	1.98203°
Longitude	114.53503°
Altitude	33,655.695 km
Speed	3.164 km/s
True Right ascension	04h 31m 43s
True Declination	1° 58' 48"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	1.13708°
Longitude	107.58798°
Altitude	33,666.87 km
Speed	3.163 km/s
Apparent Right ascension	03h 40m 14s
Apparent Declination	-4° 24' 49"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	11:50:19
Azimuth	288.72° WNW
Elevation	-27.418°
Doppler factor	1

Orbital elements

Apogee altitude	34,100.727 km
Perigee altitude	33,645.206 km
Semi-major axis	40,251.104 km
Eccentricity	0.0056585
Inclination	7.0997°
RAAN	51.9157°
Arg. of periapsis	35.811°
True anomaly	340.31788°
Mean anomaly	340.5354°
Eccentric anomaly	340.42679°
Mean motion	0.26877 °/min
BSTAR	Unknown
Orbital period	1339.45 mins