OPS 9323 (IDSCS 10), 2650
Orbit data source: Space-Track
OPS 9323 (IDSCS 10), 2650 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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2650 intel report (Beta)
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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: 19 hours ago
TLE from 19 hours ago
0 OPS 9323 (IDSCS 10)
1 02650U 67003C 26138.41246704 -.00000091 00000-0 00000-0 0 9998
2 02650 8.2366 45.0293 0033113 110.7715 81.2577 1.08222154140129Epoch: 2026-05-18T09:53Z
TLE epoch observation values (Epoch: 2026-05-18T09:53:57.152Z)
Latitude
-1.78552°
Longitude
-147.27556°
Altitude
33,675.378 km
Speed
3.155 km/s
True Right ascension
15h 49m 15s
True Declination
-1° 47' 01"
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
13:18:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,829.193 km
Perigee altitude
33,563.795 km
Semi-major axis
40,074.631 km
Eccentricity
0.00331
Inclination
8.2366°
RAAN
45.0293°
Arg. of periapsis
110.7715°
True anomaly
81.63297°
Mean anomaly
81.2577°
Eccentric anomaly
81.44531°
Mean motion
0.27054 °/min
Orbital period
1,330.65 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 9323 (IDSCS 10) 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 | 2026-05-19 04:31:38.503Z | 212.741° SW | 2026-05-19 23:52:38.503Z | 174.854° S | 38.499° | 2026-05-20 04:31:38.503Z | 165.642° S |
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2650 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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