LEMUR 2 EMBRIONOVIS, 56970
Orbit data source: Space-Track
LEMUR 2 EMBRIONOVIS, 56970 is an American payload satellite in SSO that was launched on Mon, 12 Jun 2023 UTC via an FALCON 9 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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56970 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.077 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEMUR 2 EMBRIONOVIS
1 56970U 23084AQ 26206.65264473 .00014028 00000-0 37118-3 0 9995
2 56970 97.6327 352.3651 0009095 169.1755 190.9687 15.38469249173591Epoch: 2026-07-25T15:39Z
TLE epoch observation values (Epoch: 2026-07-25T15:39:48.504Z)
Latitude
-0.00003°
Longitude
174.05116°
Altitude
459.843 km
Speed
7.633 km/s
True Right ascension
23h 29m 27s
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
05:18:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.794 km
Perigee altitude
441.378 km
Semi-major axis
6,825.723 km
Eccentricity
0.00091
Inclination
97.6327°
RAAN
352.3651°
Arg. of periapsis
169.1755°
True anomaly
190.94889°
Mean anomaly
190.9687°
Eccentric anomaly
190.95879°
Mean motion
3.84875 °/min
Orbital period
93.54 mins
BSTAR
0.00037118
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Other satellites on launch #84 in the year 2023 (2023-06-12 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.LEMUR 2 EMBRIONOVIS 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-26 21:54:16.288Z | 57.875° ENE | 2026-07-26 21:56:16.288Z | 102.205° ESE | 17.996° | 2026-07-26 21:58:16.288Z | 140.85° SSE |
| 5 mins | 2026-07-27 09:57:16.288Z | 180.693° SSW | 2026-07-27 09:59:16.288Z | 295.224° NW | 41.958° | 2026-07-27 10:02:16.288Z | 342.529° N |
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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