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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 OPS 9328 (IDSCS 15)
1 02655U 67003H 25257.21989144 -.00000063 00000-0 00000-0 0 9993
2 02655 7.5162 50.3572 0072714 32.7101 143.0841 1.07229286136242Epoch: 2025-09-14T05:16Z
TLE epoch observation values (Epoch: 2025-09-14T05:16:38.62Z)
Latitude
0.49749°
Longitude
154.06836°
Altitude
34,175.971 km
Speed
3.126 km/s
True Right ascension
15h 06m 41s
True Declination
0° 29' 49"
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
15:00:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,236.677 km
Perigee altitude
33,650.287 km
Semi-major axis
40,321.619 km
Eccentricity
0.00727
Inclination
7.5162°
RAAN
50.3572°
Arg. of periapsis
32.7101°
True anomaly
143.58096°
Mean anomaly
143.0841°
Eccentric anomaly
143.33289°
Mean motion
0.26806 °/min
Orbital period
1,342.97 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 | 2025-09-17 22:12:09.416Z | 192.509° SSW | 2025-09-18 15:17:09.416Z | 162.154° S | 37.676° | 2025-09-18 22:12:09.416Z | 155.651° 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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