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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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: 13 hours ago
TLE from 13 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 26304.53781536 .00009365 00000-0 24761-3 0 9997
2 60471 97.3716 27.1101 0003152 102.6542 257.5056 15.38627118123116Epoch: 2026-10-31T12:54Z
TLE epoch observation values (Epoch: 2026-10-31T12:54:27.247Z)
Latitude
0.00002°
Longitude
153.65446°
Altitude
453.751 km
Speed
7.64 km/s
True Right ascension
01h 48m 26s
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
21:47:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
449.259 km
Perigee altitude
444.956 km
Semi-major axis
6,825.245 km
Eccentricity
0.00032
Inclination
97.3716°
RAAN
27.1101°
Arg. of periapsis
102.6542°
True anomaly
257.47034°
Mean anomaly
257.5056°
Eccentric anomaly
257.48797°
Mean motion
3.84916 °/min
Orbital period
93.53 mins
BSTAR
0.00024761
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-01 06:13:23.841Z | 218.822° SW | 2026-11-01 06:14:23.841Z | 247.735° W | 30.846° | 2026-11-01 06:17:23.841Z | 323.664° NNW |
| 4 mins | 2026-11-01 19:08:23.841Z | 324.553° NNW | 2026-11-01 19:09:23.841Z | 296.706° NW | 27.125° | 2026-11-01 19:12:23.841Z | 229.92° WSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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