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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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: 1 day ago
TLE from 1 day ago
0 OPS 9323 (IDSCS 10)
1 02650U 67003C 26012.24503223 -.00000070 00000-0 00000-0 0 9999
2 02650 7.9997 46.1977 0032542 111.0086 243.9623 1.08221650138751Epoch: 2026-01-12T05:52Z
TLE epoch observation values (Epoch: 2026-01-12T05:52:50.784Z)
Latitude
-0.74716°
Longitude
-159.06134°
Altitude
33,752.158 km
Speed
3.149 km/s
True Right ascension
02h 43m 34s
True Declination
0° 44' 47"
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
07:01:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,827.032 km
Perigee altitude
33,566.209 km
Semi-major axis
40,074.758 km
Eccentricity
0.00325
Inclination
7.9997°
RAAN
46.1977°
Arg. of periapsis
111.0086°
True anomaly
243.62784°
Mean anomaly
243.9623°
Eccentric anomaly
243.79501°
Mean motion
0.27054 °/min
Orbital period
1,330.66 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 | 2026-01-13 06:30:49.342Z | 218.953° SW | 2026-01-14 06:30:49.342Z | 172.948° S | 38.018° | 2026-01-14 06:30:49.342Z | 172.948° 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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