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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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: 5 days ago
TLE from 5 days ago
0 OPS 9322 (IDSCS 9)
1 2649U 67003B 26086.74018219 -.00000072 00000-0 00000+0 0 9990
2 2649 8.1533 45.3106 0032722 117.9551 82.3002 1.08281302138559Epoch: 2026-03-27T17:45Z
TLE epoch observation values (Epoch: 2026-03-27T17:45:51.741Z)
Latitude
-2.85812°
Longitude
154.1325°
Altitude
33,663.253 km
Speed
3.156 km/s
True Right ascension
16h 23m 04s
True Declination
-2° 51' 18"
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
04:45:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,812.985 km
Perigee altitude
33,550.816 km
Semi-major axis
40,060.038 km
Eccentricity
0.00327
Inclination
8.1533°
RAAN
45.3106°
Arg. of periapsis
117.9551°
True anomaly
82.67199°
Mean anomaly
82.3002°
Eccentric anomaly
82.48607°
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. |
|---|---|---|---|---|---|---|---|
| 516 mins | 2026-04-01 23:04:27.334Z | 112.425° ESE | 2026-04-01 23:04:27.334Z | 112.425° ESE | 24.867° | 2026-04-02 07:40:27.334Z | 113.875° SE |
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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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