EXPLORER 36 (GEOS 2), 3093
Orbit data source: Space-Track
EXPLORER 36 (GEOS 2), 3093 is a payload satellite owned by GSFC (US) in LEO that was launched on Thu, 11 Jan 1968 UTC via a THOR DELTA E1 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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3093 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
APL
Mission
Spacecraft
Bus & Motor
ANNA, Unknown motor
Mass
212 kg wet, 212 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: 14 hours ago
TLE from 14 hours ago
0 EXPLORER 36 (GEOS 2)
1 03093U 68002A 26135.24452505 -.00000036 00000-0 13001-3 0 9993
2 03093 105.7931 14.0288 0318616 159.4028 315.0491 12.83602999733139Epoch: 2026-05-15T05:52Z
TLE epoch observation values (Epoch: 2026-05-15T05:52:06.964Z)
Latitude
63.40528°
Longitude
-92.78001°
Altitude
1,167.835 km
Speed
7.355 km/s
True Right ascension
15h 12m 54s
True Declination
63° 16' 29"
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
04:39:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,570.224 km
Perigee altitude
1,079.369 km
Semi-major axis
7,702.934 km
Eccentricity
0.03186
Inclination
105.7931°
RAAN
14.0288°
Arg. of periapsis
159.4028°
True anomaly
312.39584°
Mean anomaly
315.0491°
Eccentric anomaly
313.72996°
Mean motion
3.2104 °/min
Orbital period
112.14 mins
BSTAR
0.00013001
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Other satellites on launch #2 in the year 1968 (1968-01-11 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.EXPLORER 36 (GEOS 2) 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-05-16 04:21:59.982Z | 40.647° NE | 2026-05-16 04:27:59.982Z | 113.996° SE | 31.217° | 2026-05-16 04:32:59.982Z | 169.727° S |
| 10 mins | 2026-05-16 06:12:59.982Z | 359.834° N | 2026-05-16 06:16:59.982Z | 308.924° NW | 31.616° | 2026-05-16 06:22:59.982Z | 238.755° WSW |
| 8 mins | 2026-05-16 13:18:59.982Z | 74.694° E | 2026-05-16 13:22:59.982Z | 41.885° NE | 16.465° | 2026-05-16 13:26:59.982Z | 9.434° NNE |
| 14 mins | 2026-05-16 15:03:59.982Z | 142.633° SSE | 2026-05-16 15:10:59.982Z | 67.619° E | 43.193° | 2026-05-16 15:17:59.982Z | 343.021° N |
| 11 mins | 2026-05-16 16:55:59.982Z | 213.376° SW | 2026-05-16 17:00:59.982Z | 258.015° W | 24.295° | 2026-05-16 17:06:59.982Z | 310.227° NW |
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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