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 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: 13 hours ago
TLE from 13 hours ago
0 OPS 9328 (IDSCS 15)
1 2655U 67003H 26007.41566051 -.00000053 00000-0 00000+0 0 9995
2 2655 7.7452 49.3502 0071113 34.1970 332.4056 1.07229067137485Epoch: 2026-01-07T09:58Z
TLE epoch observation values (Epoch: 2026-01-07T09:58:33.068Z)
Latitude
0.83817°
Longitude
158.90589°
Altitude
33,687.906 km
Speed
3.164 km/s
True Right ascension
03h 42m 06s
True Declination
0° 50' 14"
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
22:40:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,230.275 km
Perigee altitude
33,656.796 km
Semi-major axis
40,321.672 km
Eccentricity
0.00711
Inclination
7.7452°
RAAN
49.3502°
Arg. of periapsis
34.197°
True anomaly
332.02514°
Mean anomaly
332.4056°
Eccentric anomaly
332.21567°
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. |
|---|---|---|---|---|---|---|---|
| 700 mins | 2026-01-08 10:50:53.975Z | 261.104° W | 2026-01-08 15:44:53.975Z | 257.198° W | 14.989° | 2026-01-08 22:30:53.975Z | 243.371° WSW |
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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
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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