OPS 9325 (IDSCS 12), 2652
Orbit data source: Space-Track
OPS 9325 (IDSCS 12), 2652 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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2652 intel report (Beta)
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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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OPS 9325 (IDSCS 12)
1 02652U 67003E 25258.77173133 -.00000086 00000-0 00000-0 0 9990
2 02652 7.7394 48.2480 0038543 75.6082 284.9222 1.07942386137150Epoch: 2025-09-15T18:31Z
TLE epoch observation values (Epoch: 2025-09-15T18:31:17.586Z)
Latitude
0.00001°
Longitude
135.54568°
Altitude
33,725.453 km
Speed
3.154 km/s
True Right ascension
03h 13m 21s
True Declination
0° 00' 00"
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
23:41:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,920.436 km
Perigee altitude
33,610.983 km
Semi-major axis
40,143.846 km
Eccentricity
0.00385
Inclination
7.7394°
RAAN
48.248°
Arg. of periapsis
75.6082°
True anomaly
284.4949°
Mean anomaly
284.9222°
Eccentric anomaly
284.7086°
Mean motion
0.26985 °/min
Orbital period
1,334.1 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 9325 (IDSCS 12) 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. |
|---|---|---|---|---|---|---|---|
| 886 mins | 2025-09-17 16:10:06.849Z | 256.701° W | 2025-09-17 22:57:06.849Z | 252.926° W | 18.442° | 2025-09-18 06:56:06.849Z | 235.719° WSW |
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2652 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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