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LEMUR 2 TOMATOKECHUP, 60471

Orbit data source: Space-Track

LEMUR 2 TOMATOKECHUP, 60471 is an American payload satellite in SSO that was launched on Fri, 16 Aug 2024 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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Identifier
60471, 2024-149D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
2024-08-16 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 4 Pan, 1.4 m
Radar Cross Section
0.326 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D   25360.18017828  .00012804  00000-0  42159-3 0  9998
2 60471  97.3961  77.2037 0002964 119.9093 240.2443 15.31620330 75649
Epoch: 2025-12-26T04:19Z
TLE epoch observation values (Epoch: 2025-12-26T04:19:27.403Z)
Latitude
-0.00003°
Longitude
-82.58504°
Altitude
475.092 km
Speed
7.628 km/s
True Right ascension
05h 08m 48s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
11:35:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.957 km
Perigee altitude
465.898 km
Semi-major axis
6,846.064 km
Eccentricity
0.0003
Inclination
97.3961°
RAAN
77.2037°
Arg. of periapsis
119.9093°
True anomaly
240.21482°
Mean anomaly
240.2443°
Eccentric anomaly
240.22956°
Mean motion
3.83161 °/min
Orbital period
93.96 mins
BSTAR
0.00042159
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