Showing default

OPS 9324 (IDSCS 11), 2651

Orbit data source: Space-Track

OPS 9324 (IDSCS 11), 2651 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 9324 (IDSCS 11) details

Identifier	2651, 1967-003D
Orbit	GEO
Last TLE update	3 days 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 3 days ago

0 OPS 9324 (IDSCS 11)
1 02651U 67003D   24353.94741108 -.00000075  00000-0  00000-0 0  9994
2 02651   7.2363  49.9096 0034399  83.6840 258.0793  1.08104758134849

Epoch: 2024-12-18T22:44Z

Definitive object data (Epoch: 2024-12-18T22:44:16.317Z)

Latitude	-2.30278°
Longitude	-37.67099°
Altitude	33,752.538 km
Speed	3.151 km/s
True Right ascension	02h 05m 43s
True Declination	-2° 18' 01"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-7.24546°
Longitude	-105.45625°
Altitude	33,860.846 km
Speed	3.142 km/s
Apparent Right ascension	21h 50m 43s
Apparent Declination	-11° 46' 45"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	12:10:38
Azimuth	57.459° ENE
Elevation	-48.261°
Doppler factor	1

Orbital elements

Apogee altitude	33,863.46 km
Perigee altitude	33,587.555 km
Semi-major axis	40,103.645 km
Eccentricity	0.0034399
Inclination	7.2363°
RAAN	49.9096°
Arg. of periapsis	83.684°
True anomaly	257.69396°
Mean anomaly	258.0793°
Eccentric anomaly	257.8866°
Mean motion	0.27025 °/min
BSTAR	Unknown
Orbital period	1332.09 mins