OPS 9311 (IDSCS 1), 2215
Orbit data source: Space-Track
OPS 9311 (IDSCS 1), 2215 is a payload satellite owned by USAF SSD (US) in GEO that was launched on Thu, 16 Jun 1966 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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2215 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Philco-Ford WDL
Mission
Non-operational Defense Communications
Bus & Motor
IDCSP, Unknown motor
Mass
45 kg wet, 45 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Ico Poly, 0.5 m
Radar Cross Section
0.926 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OPS 9311 (IDSCS 1)
1 02215U 66053B 25256.66398369 -.00000067 00000-0 00000-0 0 9994
2 02215 8.1580 46.2049 0031320 213.8590 146.0271 1.07908173131389Epoch: 2025-09-13T15:56Z
TLE epoch observation values (Epoch: 2025-09-13T15:56:08.19Z)
Latitude
0.00001°
Longitude
174.34665°
Altitude
33,876.581 km
Speed
3.143 km/s
True Right ascension
03h 05m 05s
True Declination
0° 00' 00"
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
02:47:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,899.947 km
Perigee altitude
33,648.433 km
Semi-major axis
40,152.327 km
Eccentricity
0.00313
Inclination
8.158°
RAAN
46.2049°
Arg. of periapsis
213.859°
True anomaly
146.227°
Mean anomaly
146.0271°
Eccentric anomaly
146.12712°
Mean motion
0.26976 °/min
Orbital period
1,334.52 mins
BSTAR
0
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Other satellites on launch #53 in the year 1966 (1966-06-16 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 9311 (IDSCS 1) 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 | 2025-09-15 10:09:41.645Z | 220.77° SW | 2025-09-15 19:05:41.645Z | 217.813° SW | 35.656° | 2025-09-16 10:09:41.645Z | 186.895° SSW |
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2215 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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