Showing default

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). 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.

Not visible in the next 10 days
Identifier
2653, 1967-003F
Orbit
GEO
Last TLE update
1 day ago
Origin
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 (59 years ago)
Launch vehicle
TITAN IIIC
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Ico Poly, 0.5 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 9326 (IDSCS 13)
1 02653U 67003F   25199.01473445 -.00000105  00000-0  00000-0 0  9993
2 02653   7.5427  49.2693 0046721  55.7677 304.7036  1.07748637129090
Epoch: 2025-07-18T00:21Z
TLE epoch observation values (Epoch: 2025-07-18T00:21:13.056Z)
Latitude
-0.00001°
Longitude
107.91986°
Altitude
33,705.686 km
Speed
3.158 km/s
True Right ascension
03h 17m 11s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-3.12766°
Longitude
-47.81625°
Altitude
33,973.598 km
Speed
3.137 km/s
Apparent Right ascension
16h 28m 40s
Apparent Declination
-8° 29' 20"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
00:03:26
Azimuth
278.898° WNW
Elevation
-23.55°
Doppler factor
1
Orbital elements
Apogee altitude
34,001.598 km
Perigee altitude
33,626.036 km
Semi-major axis
40,191.954 km
Eccentricity
0.00467
Inclination
7.5427°
RAAN
49.2693°
Arg. of periapsis
55.7677°
True anomaly
304.26199°
Mean anomaly
304.7036°
Eccentric anomaly
304.48294°
Mean motion
0.26936 °/min
Orbital period
1,336.5 mins
BSTAR
0
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
|