LANDSAT 8, 39084
Orbit data source: Space-Track
LANDSAT 8, 39084 is a payload satellite owned by USGS EROS (US) in SSO that was launched on Mon, 11 Feb 2013 UTC via an ATLAS V 401 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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39084 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
OSC-Gilbert
Mission
Operational Civil Imaging
Bus & Motor
LEOSTAR-3, Unknown motor
Mass
2,782 kg wet, 2,387 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 1 Pan, 10.7 m
Radar Cross Section
17.735 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 LANDSAT 8
1 39084U 13008A 26093.86191760 .00000515 00000-0 12425-3 0 9992
2 39084 98.1875 165.1687 0001220 89.4800 270.6538 14.57109763687074Epoch: 2026-04-03T20:41Z
TLE epoch observation values (Epoch: 2026-04-03T20:41:09.680Z)
Latitude
-0.00007°
Longitude
22.68841°
Altitude
705.494 km
Speed
7.503 km/s
True Right ascension
11h 00m 40s
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
12:23:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
700.47 km
Perigee altitude
698.743 km
Semi-major axis
7,077.743 km
Eccentricity
0.00012
Inclination
98.1875°
RAAN
165.1687°
Arg. of periapsis
89.48°
True anomaly
270.63982°
Mean anomaly
270.6538°
Eccentric anomaly
270.64681°
Mean motion
3.64503 °/min
Orbital period
98.76 mins
BSTAR
0.00012425
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Other satellites on launch #8 in the year 2013 (2013-02-11 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.LANDSAT 8 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-04 17:02:11.095Z | 29.472° NE | 2026-04-04 17:06:11.095Z | 90.83° ESE | 32.563° | 2026-04-04 17:10:11.095Z | 164.615° S |
| 5 mins | 2026-04-04 18:42:11.095Z | 322.129° NNW | 2026-04-04 18:44:11.095Z | 288.509° WNW | 19.567° | 2026-04-04 18:47:11.095Z | 247.773° W |
| 7 mins | 2026-04-05 04:08:11.095Z | 134.182° SE | 2026-04-05 04:11:11.095Z | 82.256° E | 32.831° | 2026-04-05 04:15:11.095Z | 5.828° NNE |
| 5 mins | 2026-04-05 05:47:11.095Z | 232.518° WSW | 2026-04-05 05:49:11.095Z | 262.774° W | 18.516° | 2026-04-05 05:52:11.095Z | 306.934° 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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