OPS 9317 (IDSCS 7), 2221
Orbit data source: Space-Track
OPS 9317 (IDSCS 7), 2221 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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2221 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 9317 (IDSCS 7)
1 02221U 66053H 25305.31466086 -.00000112 00000-0 00000-0 0 9991
2 02221 7.9904 49.1035 0082928 169.2134 190.9338 1.06869936 48592Epoch: 2025-11-01T07:33Z
TLE epoch observation values (Epoch: 2025-11-01T07:33:06.698Z)
Latitude
0°
Longitude
-105.08634°
Altitude
34,362.786 km
Speed
3.115 km/s
True Right ascension
03h 16m 09s
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
05:11:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,368.939 km
Perigee altitude
33,698.683 km
Semi-major axis
40,411.948 km
Eccentricity
0.00829
Inclination
7.9904°
RAAN
49.1035°
Arg. of periapsis
169.2134°
True anomaly
190.75537°
Mean anomaly
190.9338°
Eccentric anomaly
190.84441°
Mean motion
0.26716 °/min
Orbital period
1,347.49 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 9317 (IDSCS 7) 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 | 2025-11-02 09:23:55.128Z | 139.955° SSE | 2025-11-02 10:35:55.128Z | 137.391° SSE | 34.661° | 2025-11-03 09:23:55.128Z | 113.127° SE |
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2221 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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