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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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: 3 days ago
TLE from 3 days ago
0 OPS 9325 (IDSCS 12)
1 02652U 67003E 26205.03208014 -.00000125 00000-0 00000-0 0 9993
2 02652 8.3289 45.3817 0038479 82.2199 278.2519 1.07944170140515Epoch: 2026-07-24T00:46Z
TLE epoch observation values (Epoch: 2026-07-24T00:46:11.724Z)
Latitude
-0°
Longitude
92.1063°
Altitude
33,741.699 km
Speed
3.153 km/s
True Right ascension
03h 01m 40s
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
10:53:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,919.73 km
Perigee altitude
33,610.794 km
Semi-major axis
40,143.399 km
Eccentricity
0.00385
Inclination
8.3289°
RAAN
45.3817°
Arg. of periapsis
82.2199°
True anomaly
277.81523°
Mean anomaly
278.2519°
Eccentric anomaly
278.0336°
Mean motion
0.26985 °/min
Orbital period
1,334.08 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 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. |
|---|---|---|---|---|---|---|---|
| 313 mins | 2026-07-27 16:22:10.542Z | 248.642° W | 2026-07-27 21:35:10.542Z | 252.63° W | 20.645° | 2026-07-27 21:35:10.542Z | 252.63° W |
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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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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