Showing default

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.

Loading next visibility...
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 (2 years 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   26283.91898513  .00030557  00000-0  81187-3 0  9991
2 60471  97.3736   6.3895 0002404 142.0607 218.0808 15.38208445119947
Epoch: 2026-10-10T22:03Z
TLE epoch observation values (Epoch: 2026-10-10T22:03:20.315Z)
Latitude
0.00001°
Longitude
16.03564°
Altitude
455.816 km
Speed
7.638 km/s
True Right ascension
00h 25m 33s
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
00:34:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
449.988 km
Perigee altitude
446.706 km
Semi-major axis
6,826.484 km
Eccentricity
0.00024
Inclination
97.3736°
RAAN
6.3895°
Arg. of periapsis
142.0607°
True anomaly
218.06381°
Mean anomaly
218.0808°
Eccentric anomaly
218.07231°
Mean motion
3.84811 °/min
Orbital period
93.55 mins
BSTAR
0.00081187
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|