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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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 9314 (IDSCS 4)
1 2218U 66053E 26103.35806435 -.00000107 00000-0 00000+0 0 9997
2 2218 8.4462 45.3761 0043511 199.1632 2.3343 1.07585458234704Epoch: 2026-04-13T08:35Z
TLE epoch observation values (Epoch: 2026-04-13T08:35:36.759Z)
Latitude
-3.08748°
Longitude
-83.76677°
Altitude
33,678.474 km
Speed
3.161 km/s
True Right ascension
16h 26m 44s
True Declination
-3° 05' 03"
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
22:05:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,029.494 km
Perigee altitude
33,679.382 km
Semi-major axis
40,232.575 km
Eccentricity
0.00435
Inclination
8.4462°
RAAN
45.3761°
Arg. of periapsis
199.1632°
True anomaly
2.35472°
Mean anomaly
2.3343°
Eccentric anomaly
2.3445°
Mean motion
0.26895 °/min
Orbital period
1,338.52 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. |
|---|---|---|---|---|---|---|---|
| 658 mins | 2026-04-14 15:34:43.664Z | 115.387° SE | 2026-04-14 20:25:43.664Z | 104.247° ESE | 17.774° | 2026-04-15 02:32:43.664Z | 102.458° ESE |
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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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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