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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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: 23 hours ago
TLE from 23 hours ago
0 OPS 9316 (IDSCS 6)
1 02220U 66053G 26127.29387324 -.00000102 00000-0 00000-0 0 9996
2 02220 8.3953 46.5210 0065098 182.0572 28.2513 1.07157026138616Epoch: 2026-05-07T07:03Z
TLE epoch observation values (Epoch: 2026-05-07T07:03:10.647Z)
Latitude
-4.28615°
Longitude
-74.01617°
Altitude
33,728.784 km
Speed
3.162 km/s
True Right ascension
17h 07m 40s
True Declination
-4° 16' 54"
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
14:25:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,224.203 km
Perigee altitude
33,698.995 km
Semi-major axis
40,339.736 km
Eccentricity
0.00651
Inclination
8.3953°
RAAN
46.521°
Arg. of periapsis
182.0572°
True anomaly
28.60694°
Mean anomaly
28.2513°
Eccentric anomaly
28.42887°
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. |
|---|---|---|---|---|---|---|---|
| 82 mins | 2026-05-08 06:21:37.903Z | 118.455° SE | 2026-05-08 06:21:37.903Z | 118.455° SE | 12.352° | 2026-05-08 07:43:37.903Z | 118.446° SE |
| 490 mins | 2026-05-08 14:04:37.903Z | 109.053° ESE | 2026-05-08 18:30:37.903Z | 99.626° ESE | 13.256° | 2026-05-08 22:14:37.903Z | 96.61° ESE |
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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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