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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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 9312 (IDSCS 2)
1 2216U 66053C 26086.59973199 -.00000098 00000-0 00000+0 0 9992
2 2216 8.5091 44.6176 0032818 219.2271 341.9420 1.07850221 48382Epoch: 2026-03-27T14:23Z
TLE epoch observation values (Epoch: 2026-03-27T14:23:36.843Z)
Latitude
-3.04195°
Longitude
-155.45561°
Altitude
33,662.573 km
Speed
3.16 km/s
True Right ascension
16h 21m 55s
True Declination
-3° 02' 19"
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
19:16:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,920.388 km
Perigee altitude
33,656.75 km
Semi-major axis
40,166.706 km
Eccentricity
0.00328
Inclination
8.5091°
RAAN
44.6176°
Arg. of periapsis
219.2271°
True anomaly
341.82497°
Mean anomaly
341.942°
Eccentric anomaly
341.88353°
Mean motion
0.26961 °/min
Orbital period
1,335.24 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. |
|---|---|---|---|---|---|---|---|
| 1305 mins | 2026-03-30 13:45:01.991Z | 141.677° SSE | 2026-03-30 23:01:01.991Z | 119.851° SE | 28.928° | 2026-03-31 11:30:01.991Z | 119.636° SE |
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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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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