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, 1.0 m
Radar Cross Section
0.326 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 25258.48684505 .00010963 00000-0 39789-3 0 9998
2 60471 97.4058 335.8956 0003257 123.5220 236.6331 15.28486270 60096Epoch: 2025-09-15T11:41Z
TLE epoch observation values (Epoch: 2025-09-15T11:41:03.412Z)
Latitude
-0.00004°
Longitude
165.94059°
Altitude
484.668 km
Speed
7.622 km/s
True Right ascension
22h 23m 34s
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
16:15:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.524 km
Perigee altitude
475.058 km
Semi-major axis
6,855.428 km
Eccentricity
0.00033
Inclination
97.4058°
RAAN
335.8956°
Arg. of periapsis
123.522°
True anomaly
236.60194°
Mean anomaly
236.6331°
Eccentric anomaly
236.61752°
Mean motion
3.82377 °/min
Orbital period
94.15 mins
BSTAR
0.00039789
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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 | 2025-09-16 05:05:55.766Z | 153.723° SSE | 2025-09-16 05:08:55.766Z | 53.996° ENE | 40.629° | 2025-09-16 05:11:55.766Z | 356.109° N |
| 5 mins | 2025-09-16 18:06:55.766Z | 14.238° NNE | 2025-09-16 18:08:55.766Z | 170.125° S | 44.502° | 2025-09-16 18:11:55.766Z | 191.402° SSW |
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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