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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 25339.20492594 .00020593 00000-0 68783-3 0 9999
2 60471 97.3996 56.2775 0001711 167.8272 192.3011 15.31054679 72432Epoch: 2025-12-05T04:55Z
TLE epoch observation values (Epoch: 2025-12-05T04:55:05.601Z)
Latitude
0.00002°
Longitude
-91.7462°
Altitude
476.915 km
Speed
7.627 km/s
True Right ascension
03h 45m 06s
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
19:47:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.787 km
Perigee altitude
468.444 km
Semi-major axis
6,847.752 km
Eccentricity
0.00017
Inclination
97.3996°
RAAN
56.2775°
Arg. of periapsis
167.8272°
True anomaly
192.29692°
Mean anomaly
192.3011°
Eccentric anomaly
192.29901°
Mean motion
3.8302 °/min
Orbital period
93.99 mins
BSTAR
0.00068783
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LEMUR 2 TOMATOKECHUP Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-06 04:35:25.582Z | 118.749° SE | 2025-12-06 04:38:25.582Z | 57.368° ENE | 19.459° | 2025-12-06 04:40:25.582Z | 21.519° NNE |
| 4 mins | 2025-12-06 06:09:25.582Z | 230.1° WSW | 2025-12-06 06:11:25.582Z | 274.472° WNW | 18.513° | 2025-12-06 06:13:25.582Z | 311.17° NW |
| 4 mins | 2025-12-06 17:35:25.582Z | 67.172° ENE | 2025-12-06 17:36:25.582Z | 95.77° ESE | 24.045° | 2025-12-06 17:39:25.582Z | 155.746° SSE |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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