OPS 9314 (IDSCS 4), 2218
Orbit data source: Space-Track
OPS 9314 (IDSCS 4), 2218 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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2218 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: 1 day ago
TLE from 1 day ago
0 OPS 9314 (IDSCS 4)
1 02218U 66053E 25260.12176450 -.00000088 00000-0 00000-0 0 9991
2 02218 8.0517 47.2812 0045225 190.6188 355.9572 1.07584451232469Epoch: 2025-09-17T02:55Z
TLE epoch observation values (Epoch: 2025-09-17T02:55:20.452Z)
Latitude
-0.89996°
Longitude
-166.38124°
Altitude
33,672.274 km
Speed
3.162 km/s
True Right ascension
15h 35m 01s
True Declination
0° 53' 56"
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
00:57:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,036.645 km
Perigee altitude
33,672.739 km
Semi-major axis
40,232.829 km
Eccentricity
0.00452
Inclination
8.0517°
RAAN
47.2812°
Arg. of periapsis
190.6188°
True anomaly
355.92046°
Mean anomaly
355.9572°
Eccentric anomaly
355.93885°
Mean motion
0.26895 °/min
Orbital period
1,338.54 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 9314 (IDSCS 4) 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 | 2025-09-18 08:07:44.707Z | 215.804° SW | 2025-09-18 18:29:44.707Z | 211.654° SW | 36.582° | 2025-09-19 08:07:44.707Z | 183.09° SSW |
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2218 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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