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
ICO POLY, 0.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 OPS 9315 (IDSCS 5)
1 02219U 66053F 26236.64693469 -.00000080 00000-0 00000-0 0 9999
2 02219 8.6856 44.6249 0053621 192.2761 167.7226 1.07398362 57263Epoch: 2026-08-24T15:31Z
TLE epoch observation values (Epoch: 2026-08-24T15:31:35.157Z)
Latitude
0°
Longitude
-161.07831°
Altitude
34,109.627 km
Speed
3.13 km/s
True Right ascension
02h 58m 58s
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
01:16:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,117.127 km
Perigee altitude
33,685.164 km
Semi-major axis
40,279.282 km
Eccentricity
0.00536
Inclination
8.6856°
RAAN
44.6249°
Arg. of periapsis
192.2761°
True anomaly
167.85241°
Mean anomaly
167.7226°
Eccentric anomaly
167.78759°
Mean motion
0.26849 °/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. |
|---|---|---|---|---|---|---|---|
| 947 mins | 2026-09-11 08:55:33.807Z | 127.29° SE | 2026-09-11 12:14:33.807Z | 119.347° SE | 33.585° | 2026-09-12 00:42:33.807Z | 119.725° SE |
| 282 mins | 2026-09-12 04:13:33.807Z | 114.033° SE | 2026-09-12 08:55:33.807Z | 103.099° ESE | 14.803° | 2026-09-12 08:55:33.807Z | 103.099° ESE |
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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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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