OPS 9322 (IDSCS 9), 2649
Orbit data source: Space-Track
OPS 9322 (IDSCS 9), 2649 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.
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Philco-Ford WDL
Mission
Non-operational spacecraft
Bus & Motor
IDCSP, Unknown motor
Mass
45 kg wet, 45 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 OPS 9322 (IDSCS 9)
1 02649U 67003B 25340.46332993 -.00000062 00000-0 00000-0 0 9999
2 02649 7.9452 46.3349 0033988 117.7103 263.1241 1.08281396137356Epoch: 2025-12-06T11:07Z
TLE epoch observation values (Epoch: 2025-12-06T11:07:11.705Z)
Latitude
2.78989°
Longitude
-175.69176°
Altitude
33,696.57 km
Speed
3.153 km/s
True Right ascension
04h 26m 23s
True Declination
2° 47' 13"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
05:24:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,818.035 km
Perigee altitude
33,545.723 km
Semi-major axis
40,060.016 km
Eccentricity
0.0034
Inclination
7.9452°
RAAN
46.3349°
Arg. of periapsis
117.7103°
True anomaly
262.73763°
Mean anomaly
263.1241°
Eccentric anomaly
262.93084°
Mean motion
0.27069 °/min
Orbital period
1,329.92 mins
BSTAR
0
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Other satellites on launch #3 in the year 1967 (1967-01-18 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OPS 9322 (IDSCS 9) Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-12-07 07:19:38.663Z | 236.995° WSW | 2025-12-08 07:19:38.663Z | 207.399° SW | 34.148° | 2025-12-08 07:19:38.663Z | 207.399° SW |
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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