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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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: 1 day ago
TLE from 1 day ago
0 OPS 9313 (IDSCS 3)
1 02217U 66053D 26035.96744601 -.00000116 00000-0 00000-0 0 9994
2 02217 8.3920 45.4136 0037268 209.4606 150.4264 1.07754890138096Epoch: 2026-02-04T23:13Z
TLE epoch observation values (Epoch: 2026-02-04T23:13:07.335Z)
Latitude
0.00001°
Longitude
-77.87568°
Altitude
33,940.455 km
Speed
3.139 km/s
True Right ascension
03h 02m 07s
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
08:36:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,962.037 km
Perigee altitude
33,662.474 km
Semi-major axis
40,190.392 km
Eccentricity
0.00373
Inclination
8.392°
RAAN
45.4136°
Arg. of periapsis
209.4606°
True anomaly
150.63632°
Mean anomaly
150.4264°
Eccentric anomaly
150.53145°
Mean motion
0.26938 °/min
Orbital period
1,336.42 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. |
|---|---|---|---|---|---|---|---|
| 133 mins | 2026-02-06 06:31:26.408Z | 104.979° ESE | 2026-02-06 06:31:26.408Z | 104.979° ESE | 14.93° | 2026-02-06 08:44:26.408Z | 107.204° ESE |
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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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