OPS 9327 (IDSCS 14), 2654
Orbit data source: Space-Track
OPS 9327 (IDSCS 14), 2654 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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2654 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 9327 (IDSCS 14)
1 02654U 67003G 26095.50294346 -.00000056 00000-0 00000-0 0 9990
2 02654 8.0204 47.7721 0056567 46.7543 68.2718 1.07510571138695Epoch: 2026-04-05T12:04Z
TLE epoch observation values (Epoch: 2026-04-05T12:04:14.314Z)
Latitude
7.21709°
Longitude
148.76053°
Altitude
33,788.583 km
Speed
3.154 km/s
True Right ascension
10h 54m 30s
True Declination
7° 12' 34"
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
20:46:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,100.81 km
Perigee altitude
33,645.432 km
Semi-major axis
40,251.258 km
Eccentricity
0.00566
Inclination
8.0204°
RAAN
47.7721°
Arg. of periapsis
46.7543°
True anomaly
68.87552°
Mean anomaly
68.2718°
Eccentric anomaly
68.57351°
Mean motion
0.26877 °/min
Orbital period
1,339.46 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 9327 (IDSCS 14) 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 | 2026-04-08 14:39:52.610Z | 213.648° SW | 2026-04-09 04:23:52.610Z | 199.012° SSW | 37.816° | 2026-04-09 14:39:52.610Z | 180.437° SSW |
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2654 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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