OPS 9316 (IDSCS 6), 2220
Orbit data source: Space-Track
OPS 9316 (IDSCS 6), 2220 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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2220 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 9316 (IDSCS 6)
1 2220U 66053G 26037.16868134 -.00000095 00000-0 00000+0 0 9995
2 2220 8.2196 47.3682 0066340 180.5256 181.0784 1.07156596137651Epoch: 2026-02-06T04:02Z
TLE epoch observation values (Epoch: 2026-02-06T04:02:54.067Z)
Latitude
0.21412°
Longitude
-148.07511°
Altitude
34,226.48 km
Speed
3.123 km/s
True Right ascension
03h 15m 50s
True Declination
0° 12' 50"
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
06:36:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,229.323 km
Perigee altitude
33,694.094 km
Semi-major axis
40,339.845 km
Eccentricity
0.00663
Inclination
8.2196°
RAAN
47.3682°
Arg. of periapsis
180.5256°
True anomaly
181.06421°
Mean anomaly
181.0784°
Eccentric anomaly
181.07129°
Mean motion
0.26788 °/min
Orbital period
1,343.88 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 9316 (IDSCS 6) 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 | 2026-02-07 04:27:38.021Z | 209.952° SW | 2026-02-08 04:27:38.021Z | 168.81° S | 37.851° | 2026-02-08 04:27:38.021Z | 168.81° S |
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2220 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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