LEMUR 2 SQUIRRELCOMM, 60578
Orbit data source: Space-Track
LEMUR 2 SQUIRRELCOMM, 60578 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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60578 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 LEMUR 2 SQUIRRELCOMM
1 60578U 24149DQ 26260.51210157 .00005685 00000-0 37304-3 0 9998
2 60578 97.6651 341.1629 0006644 97.1602 263.0381 15.08039391114315Epoch: 2026-09-17T12:17Z
TLE epoch observation values (Epoch: 2026-09-17T12:17:25.575Z)
Latitude
-0.00008°
Longitude
160.35807°
Altitude
545.819 km
Speed
7.589 km/s
True Right ascension
22h 44m 39s
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
13:21:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.781 km
Perigee altitude
534.589 km
Semi-major axis
6,917.322 km
Eccentricity
0.00066
Inclination
97.6651°
RAAN
341.1629°
Arg. of periapsis
97.1602°
True anomaly
262.96253°
Mean anomaly
263.0381°
Eccentric anomaly
263.00032°
Mean motion
3.77256 °/min
Orbital period
95.43 mins
BSTAR
0.00037304
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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 SQUIRRELCOMM 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 | 2026-09-18 05:56:24.195Z | 197.742° SSW | 2026-09-18 05:58:24.195Z | 241.131° WSW | 40.041° | 2026-09-18 06:02:24.195Z | 332.446° NNW |
| 4 mins | 2026-09-18 17:33:24.195Z | 67.439° ENE | 2026-09-18 17:34:24.195Z | 88.055° E | 20.931° | 2026-09-18 17:37:24.195Z | 142.446° SSE |
| 5 mins | 2026-09-18 19:07:24.195Z | 330.144° NNW | 2026-09-18 19:09:24.195Z | 285.155° WNW | 25.426° | 2026-09-18 19:12:24.195Z | 234.029° 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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