OPS 9328 (IDSCS 15), 2655
Orbit data source: Space-Track
OPS 9328 (IDSCS 15), 2655 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.
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2655 intel report (Beta)
OPS 9328 (IDSCS 15) details
Identifier | |
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) | |
Launch vehicle | |
Launch site | |
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 1 day ago
0 OPS 9328 (IDSCS 15)
1 02655U 67003H 24355.08166495 -.00000111 00000-0 00000-0 0 9996
2 02655 6.9875 52.6363 0072123 24.7092 317.5165 1.07230272133367
Epoch: 2024-12-20T01:57Z
Definitive object data (Epoch: 2024-12-20T01:57:35.851Z)
Latitude | -2.19104° |
Longitude | -84.12206° |
Altitude | 33,728.018 km |
Speed | 3.161 km/s |
True Right ascension | 02h 17m 43s |
True Declination | -2° 11' 19" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -0.42895° |
Longitude | 117.49367° |
Altitude | 34,213.241 km |
Speed | 3.123 km/s |
Apparent Right ascension | 16h 09m 09s |
Apparent Declination | -6° 31' 40" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 11:51:43 |
Azimuth | 112.064° ESE |
Elevation | 14.88° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 34,234.049 km |
Perigee altitude | 33,652.429 km |
Semi-major axis | 40,321.376 km |
Eccentricity | 0.0072123 |
Inclination | 6.9875° |
RAAN | 52.6363° |
Arg. of periapsis | 24.7092° |
True anomaly | 316.9546° |
Mean anomaly | 317.5165° |
Eccentric anomaly | 317.23592° |
Mean motion | 0.26807 °/min |
BSTAR | Unknown |
Orbital period | 1342.96 mins |
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Other satellites on launch #3 in the year 1967 (1967-01-18 UTC)
OPS 9328 (IDSCS 15) 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. |
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156 mins | 2024-12-21 12:49:51.729Z | 112.079° ESE | 2024-12-21 12:49:51.729Z | 112.079° ESE | 14.395° | 2024-12-21 15:25:51.729Z | 114.021° SE |
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