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, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 OPS 9325 (IDSCS 12)
1 02652U 67003E 26253.20346773 -.00000079 00000-0 00000-0 0 9998
2 02652 8.4195 44.8994 0037810 85.3583 275.2003 1.07942290141035Epoch: 2026-09-10T04:52Z
TLE epoch observation values (Epoch: 2026-09-10T04:52:59.611Z)
Latitude
-0°
Longitude
-17.47567°
Altitude
33,751.693 km
Speed
3.152 km/s
True Right ascension
03h 00m 04s
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
00:03:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,917.511 km
Perigee altitude
33,613.943 km
Semi-major axis
40,143.864 km
Eccentricity
0.00378
Inclination
8.4195°
RAAN
44.8994°
Arg. of periapsis
85.3583°
True anomaly
274.76863°
Mean anomaly
275.2003°
Eccentric anomaly
274.98448°
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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-09-18 07:15:16.170Z | 234.135° WSW | 2026-09-18 20:05:16.170Z | 231.389° WSW | 39.141° | 2026-09-19 07:15:16.170Z | 206.649° SW |
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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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