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: 2 days ago
TLE from 2 days ago
0 LEMUR 2 EMBRIONOVIS
1 56970U 23084AQ 26308.36332626 .00010936 00000-0 26748-3 0 9993
2 56970 97.6451 98.4797 0008431 165.6712 194.4774 15.40949663189246Epoch: 2026-11-04T08:43Z
TLE epoch observation values (Epoch: 2026-11-04T08:43:11.388Z)
Latitude
-0.00009°
Longitude
-75.93045°
Altitude
451.987 km
Speed
7.638 km/s
True Right ascension
06h 33m 55s
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
18:24:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
446.002 km
Perigee altitude
434.505 km
Semi-major axis
6,818.391 km
Eccentricity
0.00084
Inclination
97.6451°
RAAN
98.4797°
Arg. of periapsis
165.6712°
True anomaly
194.45327°
Mean anomaly
194.4774°
Eccentric anomaly
194.46533°
Mean motion
3.85496 °/min
Orbital period
93.39 mins
BSTAR
0.00026748
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-05 22:41:10.288Z | 30.467° NE | 2026-11-05 22:44:10.288Z | 115.021° SE | 39.18° | 2026-11-05 22:46:10.288Z | 164.65° S |
| 4 mins | 2026-11-06 10:44:10.288Z | 218.292° SW | 2026-11-06 10:45:10.288Z | 245.947° WSW | 29.589° | 2026-11-06 10:48:10.288Z | 322.191° 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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