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: 21 hours ago
TLE from 21 hours ago
0 LEMUR 2 EMBRIONOVIS
1 56970U 23084AQ 26263.66938135 .00010509 00000-0 26718-3 0 9996
2 56970 97.6412 51.7762 0007689 341.7425 18.3543 15.39787527182360Epoch: 2026-09-20T16:03Z
TLE epoch observation values (Epoch: 2026-09-20T16:03:54.548Z)
Latitude
-0.00003°
Longitude
171.23868°
Altitude
444.866 km
Speed
7.648 km/s
True Right ascension
03h 27m 06s
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
06:01:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
448.932 km
Perigee altitude
438.442 km
Semi-major axis
6,821.824 km
Eccentricity
0.00077
Inclination
97.6412°
RAAN
51.7762°
Arg. of periapsis
341.7425°
True anomaly
18.38207°
Mean anomaly
18.3543°
Eccentric anomaly
18.36818°
Mean motion
3.85205 °/min
Orbital period
93.46 mins
BSTAR
0.00026718
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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 | 2026-09-21 22:16:27.614Z | 47.774° ENE | 2026-09-21 22:18:27.614Z | 95.063° ESE | 25.962° | 2026-09-21 22:20:27.614Z | 144.423° SSE |
| 4 mins | 2026-09-22 10:19:27.614Z | 201.185° SSW | 2026-09-22 10:20:27.614Z | 237.939° WSW | 47.089° | 2026-09-22 10:23:27.614Z | 333.507° NNW |
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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