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 Defense Communications
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, 0.5 m
Radar Cross Section
0.926 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OPS 9322 (IDSCS 9)
1 02649U 67003B 25258.72497659 -.00000077 00000-0 00000-0 0 9993
2 02649 7.7901 47.0427 0035583 113.1598 83.3706 1.08281449136467Epoch: 2025-09-15T17:23Z
TLE epoch observation values (Epoch: 2025-09-15T17:23:57.977Z)
Latitude
-2.25074°
Longitude
-12.08818°
Altitude
33,664.357 km
Speed
3.156 km/s
True Right ascension
16h 15m 18s
True Declination
-2° 14' 54"
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
00:43:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,824.413 km
Perigee altitude
33,539.322 km
Semi-major axis
40,060.004 km
Eccentricity
0.00356
Inclination
7.7901°
RAAN
47.0427°
Arg. of periapsis
113.1598°
True anomaly
83.77583°
Mean anomaly
83.3706°
Eccentric anomaly
83.57319°
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
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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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2649 neighbors
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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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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