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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: 18 hours ago

TLE from 18 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D   25309.19692790  .00011784  00000-0  40748-3 0  9997
2 60471  97.4023  26.3659 0001106   5.2878 354.8374 15.30057557 67841
Epoch: 2025-11-05T04:43Z
TLE epoch observation values (Epoch: 2025-11-05T04:43:34.570Z)
Latitude
-0.00004°
Longitude
-89.2012°
Altitude
477.989 km
Speed
7.627 km/s
True Right ascension
01h 45m 27s
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
18:49:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.35 km
Perigee altitude
471.835 km
Semi-major axis
6,850.73 km
Eccentricity
0.00011
Inclination
97.4023°
RAAN
26.3659°
Arg. of periapsis
5.2878°
True anomaly
354.83626°
Mean anomaly
354.8374°
Eccentric anomaly
354.83683°
Mean motion
3.8277 °/min
Orbital period
94.05 mins
BSTAR
0.00040748
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