SOICAL (CONE), 4132
Orbit data source: Space-Track
SOICAL (CONE), 4132 is a payload satellite owned by NRL (US) in LEO that was launched on Tue, 30 Sep 1969 UTC via a THORAD SLV-2G AGENA D launch vehicle from the Air Force Western Test Range (AFWTR). 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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4132 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
SOICAL, Unknown motor
Mass
3 kg wet, 3 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: 6 hours ago
TLE from 6 hours ago
0 SOICAL (CONE)
1 4132U 69082K 26100.17813529 .00001448 00000-0 56243-3 0 9990
2 4132 69.9921 65.6477 0011323 233.0669 126.9419 14.31831671911178Epoch: 2026-04-10T04:16Z
TLE epoch observation values (Epoch: 2026-04-10T04:16:30.889Z)
Latitude
0°
Longitude
163.10347°
Altitude
792.848 km
Speed
7.455 km/s
True Right ascension
04h 22m 35s
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
16:40:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.735 km
Perigee altitude
775.516 km
Semi-major axis
7,161.762 km
Eccentricity
0.00113
Inclination
69.9921°
RAAN
65.6477°
Arg. of periapsis
233.0669°
True anomaly
127.04552°
Mean anomaly
126.9419°
Eccentric anomaly
126.99372°
Mean motion
3.58107 °/min
Orbital period
100.53 mins
BSTAR
0.00056243
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Other satellites on launch #82 in the year 1969 (1969-09-30 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.SOICAL (CONE) 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-04-10 22:50:16.428Z | 191.238° SSW | 2026-04-10 22:55:16.428Z | 79.009° E | 41.804° | 2026-04-10 22:59:16.428Z | 31.315° NE |
| 5 mins | 2026-04-11 00:36:16.428Z | 283.323° WNW | 2026-04-11 00:38:16.428Z | 310.11° NW | 17.382° | 2026-04-11 00:41:16.428Z | 347.25° N |
| 8 mins | 2026-04-11 07:39:16.428Z | 3.914° NNE | 2026-04-11 07:43:16.428Z | 65.638° ENE | 25.344° | 2026-04-11 07:47:16.428Z | 114.722° SE |
| 8 mins | 2026-04-11 09:22:16.428Z | 311.394° NW | 2026-04-11 09:25:16.428Z | 265.979° W | 30.823° | 2026-04-11 09:30:16.428Z | 188.719° SSW |
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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