OPS 9328 (IDSCS 15), 2655
Orbit data source: Space-Track
OPS 9328 (IDSCS 15), 2655 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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2655 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OPS 9328 (IDSCS 15)
1 2655U 67003H 26068.47551435 -.00000120 00000-0 00000+0 0 9993
2 2655 7.8660 48.7776 0072156 35.1332 143.3723 1.07230432138135Epoch: 2026-03-09T11:24Z
TLE epoch observation values (Epoch: 2026-03-09T11:24:44.439Z)
Latitude
0.1469°
Longitude
-110.55577°
Altitude
34,174.854 km
Speed
3.126 km/s
True Right ascension
15h 11m 11s
True Declination
0° 08' 48"
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
22:36:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,234.135 km
Perigee altitude
33,652.25 km
Semi-major axis
40,321.329 km
Eccentricity
0.00722
Inclination
7.866°
RAAN
48.7776°
Arg. of periapsis
35.1332°
True anomaly
143.86206°
Mean anomaly
143.3723°
Eccentric anomaly
143.61753°
Mean motion
0.26807 °/min
Orbital period
1,342.96 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 9328 (IDSCS 15) 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 | 2026-03-09 18:26:40.160Z | 178.944° S | 2026-03-10 03:42:40.160Z | 159.024° S | 37.623° | 2026-03-10 18:26:40.160Z | 146.043° SSE |
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2655 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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