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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Edit Public Description
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: 7 hours ago
TLE from 7 hours ago
0 EXPLORER 36 (GEOS 2)
1 3093U 68002A 25318.71635670 -.00000020 00000-0 18227-3 0 9991
2 3093 105.8013 119.5128 0318062 93.8352 281.0319 12.83595863709844Epoch: 2025-11-14T17:11Z
TLE epoch observation values (Epoch: 2025-11-14T17:11:33.218Z)
Latitude
10.7925°
Longitude
164.49167°
Altitude
1,289.404 km
Speed
7.231 km/s
True Right ascension
07h 45m 44s
True Declination
10° 44' 02"
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
21:16:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,569.828 km
Perigee altitude
1,079.824 km
Semi-major axis
7,702.963 km
Eccentricity
0.03181
Inclination
105.8013°
RAAN
119.5128°
Arg. of periapsis
93.8352°
True anomaly
277.42949°
Mean anomaly
281.0319°
Eccentric anomaly
279.23315°
Mean motion
3.21038 °/min
Orbital period
112.14 mins
BSTAR
0.00018227
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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 | 2025-11-15 01:10:49.552Z | 6.207° NNE | 2025-11-15 01:16:49.552Z | 297.098° NW | 31.189° | 2025-11-15 01:21:49.552Z | 242.362° WSW |
| 4 mins | 2025-11-15 08:20:49.552Z | 62.049° ENE | 2025-11-15 08:22:49.552Z | 42.916° NE | 13.643° | 2025-11-15 08:24:49.552Z | 23.925° NE |
| 11 mins | 2025-11-15 10:05:49.552Z | 143.388° SSE | 2025-11-15 10:10:49.552Z | 89.354° E | 42.917° | 2025-11-15 10:16:49.552Z | 343.361° N |
| 8 mins | 2025-11-15 11:57:49.552Z | 223.296° SW | 2025-11-15 12:01:49.552Z | 263.84° W | 19.322° | 2025-11-15 12:05:49.552Z | 302.14° NW |
| 11 mins | 2025-11-15 23:40:49.552Z | 38.363° NE | 2025-11-15 23:45:49.552Z | 119.83° SE | 38.889° | 2025-11-15 23:51:49.552Z | 184.279° 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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