OPS 9313 (IDSCS 3), 2217
Orbit data source: Space-Track
OPS 9313 (IDSCS 3), 2217 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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2217 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: 2 days ago
TLE from 2 days ago
0 OPS 9313 (IDSCS 3)
1 02217U 66053D 26138.97385162 -.00000063 00000-0 00000-0 0 9993
2 02217 8.5851 44.4426 0035573 210.8956 148.7658 1.07753366139201Epoch: 2026-05-18T23:22Z
TLE epoch observation values (Epoch: 2026-05-18T23:22:20.779Z)
Latitude
0.00001°
Longitude
177.07678°
Altitude
33,934.134 km
Speed
3.14 km/s
True Right ascension
02h 57m 16s
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
23:27:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,955.603 km
Perigee altitude
33,669.662 km
Semi-major axis
40,190.77 km
Eccentricity
0.00356
Inclination
8.5851°
RAAN
44.4426°
Arg. of periapsis
210.8956°
True anomaly
148.97637°
Mean anomaly
148.7658°
Eccentric anomaly
148.87117°
Mean motion
0.26937 °/min
Orbital period
1,336.44 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 9313 (IDSCS 3) 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 | 2026-05-20 14:34:58.307Z | 220.41° SW | 2026-05-21 02:28:58.307Z | 216.142° SW | 36.224° | 2026-05-21 14:34:58.307Z | 188.565° SSW |
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2217 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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