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: 1 day ago
TLE from 1 day ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 25288.19963357 .00012518 00000-0 44099-3 0 9992
2 60471 97.4029 5.4561 0002666 60.5865 299.5641 15.29432483 64638Epoch: 2025-10-15T04:47Z
TLE epoch observation values (Epoch: 2025-10-15T04:47:28.340Z)
Latitude
-0.00003°
Longitude
-90.38911°
Altitude
479.709 km
Speed
7.626 km/s
True Right ascension
00h 21m 49s
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
02:12:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.288 km
Perigee altitude
472.634 km
Semi-major axis
6,852.598 km
Eccentricity
0.00027
Inclination
97.4029°
RAAN
5.4561°
Arg. of periapsis
60.5865°
True anomaly
299.53752°
Mean anomaly
299.5641°
Eccentric anomaly
299.55081°
Mean motion
3.82614 °/min
Orbital period
94.09 mins
BSTAR
0.00044099
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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 | 2025-10-16 17:28:31.132Z | 42.156° NE | 2025-10-16 17:31:31.132Z | 105.737° ESE | 22.256° | 2025-10-16 17:33:31.132Z | 146.301° SSE |
| 5 mins | 2025-10-17 05:36:31.132Z | 193.731° SSW | 2025-10-17 05:38:31.132Z | 269.36° W | 37.567° | 2025-10-17 05:41:31.132Z | 336.11° NNW |
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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