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: 3 days ago
TLE from 3 days ago
0 OPS 9328 (IDSCS 15)
1 02655U 67003H 26155.26384414 -.00000114 00000-0 00000-0 0 9992
2 02655 8.0364 47.9764 0073500 38.2397 164.5711 1.07230572139066Epoch: 2026-06-04T06:19Z
TLE epoch observation values (Epoch: 2026-06-04T06:19:56.133Z)
Latitude
-3.15717°
Longitude
-96.8837°
Altitude
34,229.226 km
Speed
3.122 km/s
True Right ascension
16h 43m 14s
True Declination
-3° 09' 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
11:23:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,239.517 km
Perigee altitude
33,646.794 km
Semi-major axis
40,321.293 km
Eccentricity
0.00735
Inclination
8.0364°
RAAN
47.9764°
Arg. of periapsis
38.2397°
True anomaly
164.79321°
Mean anomaly
164.5711°
Eccentric anomaly
164.68235°
Mean motion
0.26807 °/min
Orbital period
1,342.95 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
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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. |
|---|---|---|---|---|---|---|---|
| OPS 9328 (IDSCS 15) is likely not visible in the next few days. |
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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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