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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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: 2 days ago
TLE from 2 days ago
0 OPS 9327 (IDSCS 14)
1 02654U 67003G 25307.66390615 -.00000072 00000-0 00000-0 0 9996
2 02654 7.7219 49.1736 0055843 45.1001 312.2682 1.07511090137044Epoch: 2025-11-03T15:56Z
TLE epoch observation values (Epoch: 2025-11-03T15:56:01.491Z)
Latitude
-0.40802°
Longitude
123.89439°
Altitude
33,720.645 km
Speed
3.159 km/s
True Right ascension
03h 04m 15s
True Declination
0° 24' 27"
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
15:39:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,097.768 km
Perigee altitude
33,648.219 km
Semi-major axis
40,251.131 km
Eccentricity
0.00558
Inclination
7.7219°
RAAN
49.1736°
Arg. of periapsis
45.1001°
True anomaly
311.79243°
Mean anomaly
312.2682°
Eccentric anomaly
312.03054°
Mean motion
0.26877 °/min
Orbital period
1,339.45 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. |
|---|---|---|---|---|---|---|---|
| 645 mins | 2025-11-06 08:53:55.134Z | 246.562° WSW | 2025-11-06 18:39:55.134Z | 245.702° WSW | 24.509° | 2025-11-06 19:38:55.134Z | 243.543° WSW |
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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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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