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DECAYED
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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). Payloads include a variety of satellites, spacecraft, and rockets 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.

Next visibility unknown
No 3D visualization available: RSO Decayed
LEMUR 2 ROMEO-N-LEO details
Identifier
56206, 2023-054AE
Orbit
Decayed
Last TLE update5 months ago
Origin
Flag of USSpire (US)
ManufacturerSpire/Glasgow
MissionDecayed Commercial Com/MetRO
Bus & MotorCUBESAT 3U, Unknown motor
Mass4.6 kg wet, 4.6 kg dry
Launch date (UTC)
2023-04-15 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBRBox + 2 Pan, 0.7 m
Radar Cross Section0.054 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 5 months 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 58313
Epoch: 2024-04-23T12:40Z
Definitive object data (Epoch: 2024-04-23T12:40:59.369Z)
Latitude-0.00009°
Longitude-22.10182°
Altitude163.549 km
Speed7.806 km/s
True Right ascension01h 20m 47s
True Declination0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Predictive object data (real-time)
LatitudeUnknown
LongitudeUnknown
AltitudeUnknown
SpeedUnknown
Apparent Right ascensionUnknown
Apparent DeclinationUnknown
SunlitUnknown
Predictive observer data (real-time)
Local Sidereal Time16:05:36
AzimuthUnknown
ElevationUnknown
Doppler factorUnknown
Orbital elements
Apogee157.647 km
Perigee150.761 km
Semi-major axis6,532.341 km
Eccentricity0.0005271
Inclination97.3326°
RAAN20.1972°
Arg. of periapsis213.1858°
True anomaly146.94426°
Mean anomaly146.9113°
Eccentric anomaly146.92778°
Mean motion4.11093 °/min
BSTAR0.0007357
Period87.57 mins
No data available

LEMUR 2 ROMEO-N-LEO Visibility forecast

Observer location: 39.9160978°, -105.1181434

This satellite is decayed
Span
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Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.