OPS 9312 (IDSCS 2), 2216
Orbit data source: Space-Track
OPS 9312 (IDSCS 2), 2216 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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2216 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 9312 (IDSCS 2)
1 02216U 66053C 26035.08179220 -.00000122 00000-0 00000-0 0 9992
2 02216 8.4120 45.1103 0033841 217.4907 140.2369 1.07851063 47828Epoch: 2026-02-04T01:57Z
TLE epoch observation values (Epoch: 2026-02-04T01:57:46.846Z)
Latitude
-0.31124°
Longitude
-120.56836°
Altitude
33,890.959 km
Speed
3.142 km/s
True Right ascension
02h 52m 31s
True Declination
0° 18' 39"
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
13:50:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,924.288 km
Perigee altitude
33,652.433 km
Semi-major axis
40,166.498 km
Eccentricity
0.00338
Inclination
8.412°
RAAN
45.1103°
Arg. of periapsis
217.4907°
True anomaly
140.48413°
Mean anomaly
140.2369°
Eccentric anomaly
140.3606°
Mean motion
0.26962 °/min
Orbital period
1,335.23 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 9312 (IDSCS 2) 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. |
|---|---|---|---|---|---|---|---|
| 1053 mins | 2026-02-06 11:44:05.256Z | 121.952° SE | 2026-02-06 11:44:05.256Z | 121.952° SE | 16.908° | 2026-02-07 05:17:05.256Z | 98.614° ESE |
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2216 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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