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: 2 days ago
TLE from 2 days ago
0 OPS 9316 (IDSCS 6)
1 02220U 66053G 25285.45681955 -.00000084 00000-0 00000-0 0 9994
2 02220 7.9935 48.4188 0067385 175.4523 160.8448 1.07156467136390Epoch: 2025-10-12T10:57Z
TLE epoch observation values (Epoch: 2025-10-12T10:57:49.209Z)
Latitude
-3.16997°
Longitude
-160.58008°
Altitude
34,218.502 km
Speed
3.123 km/s
True Right ascension
01h 40m 35s
True Declination
-3° 09' 60"
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
00:29:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,233.573 km
Perigee altitude
33,689.912 km
Semi-major axis
40,339.88 km
Eccentricity
0.00674
Inclination
7.9935°
RAAN
48.4188°
Arg. of periapsis
175.4523°
True anomaly
161.09617°
Mean anomaly
160.8448°
Eccentric anomaly
160.97068°
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 | 2025-10-14 05:57:29.227Z | 194.511° SSW | 2025-10-14 15:02:29.227Z | 185.349° SSW | 38.403° | 2025-10-15 05:57:29.227Z | 160.422° 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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