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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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: 22 hours ago
TLE from 22 hours ago
0 OPS 9327 (IDSCS 14)
1 2654U 67003G 25354.25132412 -.00000104 00000-0 00000+0 0 9997
2 2654 7.8127 48.7668 0055131 45.4282 343.9780 1.07511685137552Epoch: 2025-12-20T06:01Z
TLE epoch observation values (Epoch: 2025-12-20T06:01:54.403Z)
Latitude
3.82882°
Longitude
-101.79425°
Altitude
33,656.497 km
Speed
3.164 km/s
True Right ascension
05h 11m 03s
True Declination
3° 49' 29"
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
03:11:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,094.752 km
Perigee altitude
33,650.937 km
Semi-major axis
40,250.982 km
Eccentricity
0.00551
Inclination
7.8127°
RAAN
48.7668°
Arg. of periapsis
45.4282°
True anomaly
343.80247°
Mean anomaly
343.978°
Eccentric anomaly
343.89035°
Mean motion
0.26877 °/min
Orbital period
1,339.44 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 | 2025-12-21 04:12:21.646Z | 138.611° SSE | 2025-12-21 06:37:21.646Z | 131.992° SE | 32.97° | 2025-12-22 04:12:21.646Z | 110.045° ESE |
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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
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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