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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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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OPS 9315 (IDSCS 5)
1 02219U 66053F 25305.56750216 -.00000040 00000-0 00000-0 0 9996
2 02219 8.1275 47.4204 0054716 184.7144 175.1997 1.07397815 54089Epoch: 2025-11-01T13:37Z
TLE epoch observation values (Epoch: 2025-11-01T13:37:12.186Z)
Latitude
0.00001°
Longitude
161.95573°
Altitude
34,120.124 km
Speed
3.129 km/s
True Right ascension
03h 09m 24s
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
21:09:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,121.68 km
Perigee altitude
33,680.894 km
Semi-major axis
40,279.424 km
Eccentricity
0.00547
Inclination
8.1275°
RAAN
47.4204°
Arg. of periapsis
184.7144°
True anomaly
175.25181°
Mean anomaly
175.1997°
Eccentric anomaly
175.22579°
Mean motion
0.26848 °/min
Orbital period
1,340.86 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 | 2025-11-04 01:15:47.724Z | 216.356° SW | 2025-11-04 15:02:47.724Z | 206.75° SW | 37.218° | 2025-11-05 01:15:47.724Z | 183.917° SSW |
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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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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