OPS 9344 (IDSCS 22), 3287
Orbit data source: Space-Track
OPS 9344 (IDSCS 22), 3287 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.
Focus sentinelFocus sentinel
3287 intel report (Beta)
OPS 9344 (IDSCS 22) details
Identifier | |
Orbit | GEO |
Last TLE update | 1 day ago |
Origin | |
Manufacturer | Philco-Ford |
Mission | Non-operational Defense Communications |
Bus & Motor | IDCSP, Unknown motor |
Mass | 45 kg wet, 45 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
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 9344 (IDSCS 22)
1 03287U 68050D 24355.25327427 -.00000072 00000-0 00000-0 0 9990
2 03287 6.0636 57.0412 0025685 133.7471 306.1898 1.07639944221412
Epoch: 2024-12-20T06:04Z
Definitive object data (Epoch: 2024-12-20T06:04:42.896Z)
Latitude | 5.98695° |
Longitude | -43.80846° |
Altitude | 33,778.198 km |
Speed | 3.153 km/s |
True Right ascension | 09h 06m 46s |
True Declination | 5° 58' 50" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -3.75019° |
Longitude | 94.37857° |
Altitude | 33,829.17 km |
Speed | 3.149 km/s |
Apparent Right ascension | 18h 46m 52s |
Apparent Declination | -9° 17' 54" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 11:56:15 |
Azimuth | 89.12° E |
Elevation | -15.634° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 33,944.18 km |
Perigee altitude | 33,737.575 km |
Semi-major axis | 40,219.015 km |
Eccentricity | 0.0025685 |
Inclination | 6.0636° |
RAAN | 57.0412° |
Arg. of periapsis | 133.7471° |
True anomaly | 305.95181° |
Mean anomaly | 306.1898° |
Eccentric anomaly | 306.07085° |
Mean motion | 0.26909 °/min |
BSTAR | Unknown |
Orbital period | 1337.85 mins |
Loading historical data...
3287 neighbors
Authenticating... |
Loading maneuver chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #50 in the year 1968 (1968-06-13 UTC)
OPS 9344 (IDSCS 22) Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
---|
Authenticating...
Click to sort rows by NORAD ID header in ascending order | Click to sort rows by Common name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
---|