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 Defense Communications
Bus & Motor
IDCSP, Unknown motor
Mass
45 kg wet, 45 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Ico Poly, 0.5 m
Radar Cross Section
0.926 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OPS 9316 (IDSCS 6)
1 02220U 66053G 25254.51411222 -.00000056 00000-0 00000-0 0 9994
2 02220 7.9327 48.6972 0066808 174.0322 105.1248 1.07156036136065Epoch: 2025-09-11T12:20Z
TLE epoch observation values (Epoch: 2025-09-11T12:20:19.295Z)
Latitude
-7.81242°
Longitude
152.80913°
Altitude
34,034.556 km
Speed
3.138 km/s
True Right ascension
21h 54m 39s
True Declination
-7° 48' 15"
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
16:48:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,231.355 km
Perigee altitude
33,692.348 km
Semi-major axis
40,339.988 km
Eccentricity
0.00668
Inclination
7.9327°
RAAN
48.6972°
Arg. of periapsis
174.0322°
True anomaly
105.86222°
Mean anomaly
105.1248°
Eccentric anomaly
105.49367°
Mean motion
0.26788 °/min
Orbital period
1,343.89 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 | 2025-09-14 00:15:56.779Z | 235.453° WSW | 2025-09-14 19:17:56.779Z | 217.066° SW | 35.661° | 2025-09-15 00:15:56.779Z | 203.705° SW |
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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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