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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60471 intel report (Beta)
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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: 19 hours ago
TLE from 19 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 25318.22103622 .00016077 00000-0 54833-3 0 9992
2 60471 97.4009 35.3563 0000476 308.1166 52.0032 15.30431220 69228Epoch: 2025-11-14T05:18Z
TLE epoch observation values (Epoch: 2025-11-14T05:18:17.529Z)
Latitude
-0°
Longitude
-97.78439°
Altitude
477.429 km
Speed
7.627 km/s
True Right ascension
02h 21m 25s
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
21:22:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.803 km
Perigee altitude
471.15 km
Semi-major axis
6,849.613 km
Eccentricity
0.00005
Inclination
97.4009°
RAAN
35.3563°
Arg. of periapsis
308.1166°
True anomaly
52.0075°
Mean anomaly
52.0032°
Eccentric anomaly
52.00535°
Mean motion
3.82864 °/min
Orbital period
94.03 mins
BSTAR
0.00054833
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-15 04:58:16.347Z | 145.083° SSE | 2025-11-15 05:01:16.347Z | 77.28° E | 34.545° | 2025-11-15 05:04:16.347Z | 3.866° NNE |
| 5 mins | 2025-11-15 17:58:16.347Z | 26.074° NE | 2025-11-15 18:00:16.347Z | 91.157° ESE | 40.639° | 2025-11-15 18:03:16.347Z | 179.4° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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