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: 3 days ago
TLE from 3 days ago
0 EXPLORER 36 (GEOS 2)
1 3093U 68002A 25312.41333176 -.00000025 00000-0 16736-3 0 9996
2 3093 105.8014 110.6756 0318048 104.0888 315.0775 12.83595542709036Epoch: 2025-11-08T09:55Z
TLE epoch observation values (Epoch: 2025-11-08T09:55:11.864Z)
Latitude
53.47793°
Longitude
-108.3126°
Altitude
1,165.892 km
Speed
7.355 km/s
True Right ascension
05h 53m 19s
True Declination
53° 19' 20"
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
23:04:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,569.818 km
Perigee altitude
1,079.836 km
Semi-major axis
7,702.964 km
Eccentricity
0.0318
Inclination
105.8014°
RAAN
110.6756°
Arg. of periapsis
104.0888°
True anomaly
312.43038°
Mean anomaly
315.0775°
Eccentric anomaly
313.7614°
Mean motion
3.21038 °/min
Orbital period
112.14 mins
BSTAR
0.00016736
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-11 08:52:24.813Z | 104.371° ESE | 2025-11-11 08:57:24.813Z | 56.511° ENE | 24.081° | 2025-11-11 09:02:24.813Z | 3.073° NNE |
| 12 mins | 2025-11-11 10:41:24.813Z | 172.396° S | 2025-11-11 10:47:24.813Z | 269.505° W | 41.34° | 2025-11-11 10:53:24.813Z | 330.225° NNW |
| 6 mins | 2025-11-11 22:28:24.813Z | 74.123° E | 2025-11-11 22:31:24.813Z | 104.56° ESE | 16.162° | 2025-11-11 22:34:24.813Z | 132.337° SE |
| 11 mins | 2025-11-12 00:16:24.813Z | 19.051° NNE | 2025-11-12 00:21:24.813Z | 272.384° WNW | 44.455° | 2025-11-12 00:27:24.813Z | 210.071° SW |
| 5 mins | 2025-11-12 02:08:24.813Z | 330.015° NNW | 2025-11-12 02:10:24.813Z | 309.333° NW | 15.049° | 2025-11-12 02:13:24.813Z | 281.62° WNW |
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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