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
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OPS 9325 (IDSCS 12)
1 02652U 67003E 26079.97215275 -.00000109 00000-0 00000-0 0 9994
2 02652 8.0957 46.5595 0036487 77.7587 282.7059 1.07943045139165Epoch: 2026-03-20T23:19Z
TLE epoch observation values (Epoch: 2026-03-20T23:19:53.997Z)
Latitude
-0.00001°
Longitude
-121.85901°
Altitude
33,732.938 km
Speed
3.154 km/s
True Right ascension
03h 06m 27s
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
10:50:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,912.015 km
Perigee altitude
33,619.071 km
Semi-major axis
40,143.68 km
Eccentricity
0.00365
Inclination
8.0957°
RAAN
46.5595°
Arg. of periapsis
77.7587°
True anomaly
282.29762°
Mean anomaly
282.7059°
Eccentric anomaly
282.5018°
Mean motion
0.26985 °/min
Orbital period
1,334.09 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 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-03-22 05:51:57.337Z | 147.786° SSE | 2026-03-22 05:51:57.337Z | 147.786° SSE | 35.321° | 2026-03-23 05:51:57.337Z | 119.119° SE |
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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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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