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
ICO POLY, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OPS 9322 (IDSCS 9)
1 02649U 67003B 26259.84628051 -.00000114 00000-0 00000-0 0 9992
2 02649 8.4696 43.6564 0034978 124.7594 238.1429 1.08282225140438Epoch: 2026-09-16T20:18Z
TLE epoch observation values (Epoch: 2026-09-16T20:18:38.636Z)
Latitude
0.36699°
Longitude
105.72213°
Altitude
33,754.796 km
Speed
3.149 km/s
True Right ascension
03h 04m 42s
True Declination
0° 21' 60"
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
00:04:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,821.792 km
Perigee altitude
33,541.549 km
Semi-major axis
40,059.808 km
Eccentricity
0.0035
Inclination
8.4696°
RAAN
43.6564°
Arg. of periapsis
124.7594°
True anomaly
237.80324°
Mean anomaly
238.1429°
Eccentric anomaly
237.97299°
Mean motion
0.27069 °/min
Orbital period
1,329.91 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
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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. |
|---|---|---|---|---|---|---|---|
| OPS 9322 (IDSCS 9) is likely not visible in the next few days. |
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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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