OPS 9315 (IDSCS 5), 2219
Orbit data source: Space-Track
OPS 9315 (IDSCS 5), 2219 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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2219 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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 OPS 9315 (IDSCS 5)
1 02219U 66053F 26147.26404164 -.00000128 00000-0 00000-0 0 9993
2 02219 8.5209 45.5068 0052155 190.8619 168.8976 1.07399369 56306Epoch: 2026-05-27T06:20Z
TLE epoch observation values (Epoch: 2026-05-27T06:20:13.197Z)
Latitude
-0.00001°
Longitude
65.50627°
Altitude
34,106.406 km
Speed
3.13 km/s
True Right ascension
03h 01m 32s
True Declination
0° 00' 00"
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
15:44:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,110.97 km
Perigee altitude
33,690.82 km
Semi-major axis
40,279.032 km
Eccentricity
0.00522
Inclination
8.5209°
RAAN
45.5068°
Arg. of periapsis
190.8619°
True anomaly
169.01195°
Mean anomaly
168.8976°
Eccentric anomaly
168.95485°
Mean motion
0.26849 °/min
Orbital period
1,340.84 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 9315 (IDSCS 5) 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 | 2026-06-04 05:54:35.868Z | 158.587° S | 2026-06-04 19:54:35.868Z | 132.284° SE | 33.745° | 2026-06-05 05:54:35.868Z | 131.215° SE |
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2219 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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