Showing default

OPS 9347 (IDSCS 25), 3290

Orbit data source: Space-Track

OPS 9347 (IDSCS 25), 3290 is a payload satellite owned by SAMSO (US) in GEO that was launched on Thu, 13 Jun 1968 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 9347 (IDSCS 25) details

Identifier	3290, 1968-050G
Orbit	GEO
Last TLE update	1 day ago
Origin	SAMSO (US)
Manufacturer	Philco-Ford
Mission	Non-operational Defense Communications
Bus & Motor	IDCSP, Unknown motor
Mass	45 kg wet, 45 kg dry
Launch date (UTC)	1968-06-13 (57 years ago)
Launch vehicle	TITAN IIIC
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	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 day ago

0 OPS 9347 (IDSCS 25)
1 03290U 68050G   24355.34424318 -.00000062  00000-0  00000-0 0  9990
2 03290   5.8220  58.8410 0059958 122.2182  46.5883  1.07034862 41317

Epoch: 2024-12-20T08:15Z

Definitive object data (Epoch: 2024-12-20T08:15:42.61Z)

Latitude	1.06966°
Longitude	14.87187°
Altitude	33,825.725 km
Speed	3.155 km/s
True Right ascension	15h 12m 50s
True Declination	1° 04' 07"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-5.83555°
Longitude	118.15517°
Altitude	34,200.78 km
Speed	3.126 km/s
Apparent Right ascension	22h 18m 54s
Apparent Declination	-10° 23' 55"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	12:09:40
Azimuth	47.394° ENE
Elevation	-51.61°
Doppler factor	1

Orbital elements

Apogee altitude	34,234.357 km
Perigee altitude	33,750.251 km
Semi-major axis	40,370.441 km
Eccentricity	0.0059958
Inclination	5.822°
RAAN	58.841°
Arg. of periapsis	122.2182°
True anomaly	47.08999°
Mean anomaly	46.5883°
Eccentric anomaly	46.83889°
Mean motion	0.26758 °/min
BSTAR	Unknown
Orbital period	1345.41 mins