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: 13 hours ago
TLE from 13 hours ago
0 LEMUR 2 SQUIRRELCOMM
1 60578U 24149DQ 26080.45463675 .00008919 00000-0 61498-3 0 9990
2 60578 97.6729 161.7069 0005133 3.3791 356.7469 15.06044190 87198Epoch: 2026-03-21T10:54Z
TLE epoch observation values (Epoch: 2026-03-21T10:54:40.615Z)
Latitude
-0.00006°
Longitude
179.06257°
Altitude
547.816 km
Speed
7.59 km/s
True Right ascension
10h 46m 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
04:27:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.852 km
Perigee altitude
541.745 km
Semi-major axis
6,923.435 km
Eccentricity
0.00051
Inclination
97.6729°
RAAN
161.7069°
Arg. of periapsis
3.3791°
True anomaly
356.74356°
Mean anomaly
356.7469°
Eccentric anomaly
356.74523°
Mean motion
3.76756 °/min
Orbital period
95.55 mins
BSTAR
0.00061498
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-22 04:35:36.751Z | 120.658° SE | 2026-03-22 04:38:36.751Z | 65.75° ENE | 21.908° | 2026-03-22 04:40:36.751Z | 26.385° NE |
| 4 mins | 2026-03-22 06:11:36.751Z | 232.989° WSW | 2026-03-22 06:12:36.751Z | 253.842° W | 20.875° | 2026-03-22 06:15:36.751Z | 312.197° NW |
| 5 mins | 2026-03-22 17:47:36.751Z | 40.052° NE | 2026-03-22 17:49:36.751Z | 90.209° ESE | 32.378° | 2026-03-22 17:52:36.751Z | 163.013° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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