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: 2 days ago
TLE from 2 days ago
0 SOICAL (CONE)
1 4132U 69082K 26171.43080274 .00000763 00000-0 30562-3 0 9995
2 4132 69.9927 263.9721 0007022 134.9363 225.2332 14.31991257921377Epoch: 2026-06-20T10:20Z
TLE epoch observation values (Epoch: 2026-06-20T10:20:21.356Z)
Latitude
-0.00006°
Longitude
-159.76244°
Altitude
790.978 km
Speed
7.457 km/s
True Right ascension
17h 35m 53s
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
07:09:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
788.121 km
Perigee altitude
778.064 km
Semi-major axis
7,161.23 km
Eccentricity
0.0007
Inclination
69.9927°
RAAN
263.9721°
Arg. of periapsis
134.9363°
True anomaly
225.17611°
Mean anomaly
225.2332°
Eccentric anomaly
225.20465°
Mean motion
3.58147 °/min
Orbital period
100.52 mins
BSTAR
0.00030562
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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 | 2026-06-23 07:12:15.896Z | 204.059° SW | 2026-06-23 07:16:15.896Z | 226.06° WSW | 44.883° | 2026-06-23 07:21:15.896Z | 24.011° NE |
| 8 mins | 2026-06-23 16:01:15.896Z | 1.639° NNE | 2026-06-23 16:04:15.896Z | 54.407° ENE | 31.649° | 2026-06-23 16:09:15.896Z | 126.602° SE |
| 7 mins | 2026-06-23 17:44:15.896Z | 299.63° NW | 2026-06-23 17:47:15.896Z | 253.314° W | 24.191° | 2026-06-23 17:51:15.896Z | 201.442° SSW |
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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