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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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: 14 hours ago
TLE from 14 hours ago
0 OPS 9324 (IDSCS 11)
1 02651U 67003D 25292.20589840 -.00000117 00000-0 00000-0 0 9996
2 02651 7.8120 47.3105 0034743 94.1835 223.9890 1.08105676138138Epoch: 2025-10-19T04:56Z
TLE epoch observation values (Epoch: 2025-10-19T04:56:29.621Z)
Latitude
-5.22071°
Longitude
-96.59715°
Altitude
33,825.2 km
Speed
3.145 km/s
True Right ascension
00h 21m 48s
True Declination
-5° 12' 55"
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
13:42:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,864.608 km
Perigee altitude
33,585.945 km
Semi-major axis
40,103.414 km
Eccentricity
0.00347
Inclination
7.812°
RAAN
47.3105°
Arg. of periapsis
94.1835°
True anomaly
223.71336°
Mean anomaly
223.989°
Eccentric anomaly
223.85109°
Mean motion
0.27025 °/min
Orbital period
1,332.08 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 | 2025-10-19 18:48:41.181Z | 144.033° SSE | 2025-10-19 18:48:41.181Z | 144.033° SSE | 30.541° | 2025-10-20 18:48:41.181Z | 118.858° 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
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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