OPS 9324 (IDSCS 11), 2651
Orbit data source: Space-Track
OPS 9324 (IDSCS 11), 2651 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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2651 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
ICO POLY, 0.5 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 9324 (IDSCS 11)
1 02651U 67003D 26206.41250720 -.00000097 00000-0 00000-0 0 9994
2 02651 8.3342 44.7473 0034726 99.6016 164.9658 1.08105359141151Epoch: 2026-07-25T09:54Z
TLE epoch observation values (Epoch: 2026-07-25T09:54:00.622Z)
Latitude
-8.32107°
Longitude
-142.26188°
Altitude
33,860.287 km
Speed
3.142 km/s
True Right ascension
20h 37m 27s
True Declination
-8° 18' 45"
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
10:56:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,864.614 km
Perigee altitude
33,586.087 km
Semi-major axis
40,103.488 km
Eccentricity
0.00347
Inclination
8.3342°
RAAN
44.7473°
Arg. of periapsis
99.6016°
True anomaly
165.06859°
Mean anomaly
164.9658°
Eccentric anomaly
165.01724°
Mean motion
0.27025 °/min
Orbital period
1,332.09 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 9324 (IDSCS 11) 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 | 2026-07-26 21:39:01.414Z | 170.438° S | 2026-07-26 21:39:01.414Z | 170.438° S | 37.799° | 2026-07-27 21:39:01.414Z | 131.229° SE |
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2651 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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