LEMUR 2 ROMEO-N-LEO, 56206 (Decayed)
Orbit data source: Space-Track
LEMUR 2 ROMEO-N-LEO, 56206 was a payload satellite owned by Spire (US) in LEO that was launched on Sat, 15 Apr 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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56206 intel report (Beta)
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LEMUR 2 ROMEO-N-LEO radio frequencies
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Decayed Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.6 kg wet, 4.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.054 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 LEMUR 2 ROMEO-N-LEO
1 56206U 23054AE 24114.52846493 .16734428 27557-5 73570-3 0 9997
2 56206 97.3326 20.1972 0005271 213.1858 146.9113 16.43162300 58313Epoch: 2024-04-23T12:40Z
TLE epoch observation values (Epoch: 2024-04-23T12:40:59.369Z)
Latitude
-0.00009°
Longitude
-22.10182°
Altitude
163.549 km
Speed
7.806 km/s
True Right ascension
01h 20m 47s
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
16:53:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
157.647 km
Perigee altitude
150.761 km
Semi-major axis
6,532.341 km
Eccentricity
0.00053
Inclination
97.3326°
RAAN
20.1972°
Arg. of periapsis
213.1858°
True anomaly
146.94426°
Mean anomaly
146.9113°
Eccentric anomaly
146.92778°
Mean motion
4.11093 °/min
Orbital period
87.57 mins
BSTAR
0.0007357
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Other satellites on launch #54 in the year 2023 (2023-04-15 UTC)
LEMUR 2 ROMEO-N-LEO Visibility
Observer location: undefined°, undefined°
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. |
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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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