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: 20 hours ago
TLE from 20 hours ago
0 LEMUR 2 SQUIRRELCOMM
1 60578U 24149DQ 26304.49826196 .00004420 00000-0 28787-3 0 9991
2 60578 97.6627 25.0351 0004070 316.5617 43.5290 15.08452725120949Epoch: 2026-10-31T11:57Z
TLE epoch observation values (Epoch: 2026-10-31T11:57:29.833Z)
Latitude
-0.00002°
Longitude
165.85768°
Altitude
541.953 km
Speed
7.592 km/s
True Right ascension
01h 40m 08s
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
03:28:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.735 km
Perigee altitude
535.105 km
Semi-major axis
6,916.057 km
Eccentricity
0.00041
Inclination
97.6627°
RAAN
25.0351°
Arg. of periapsis
316.5617°
True anomaly
43.56113°
Mean anomaly
43.529°
Eccentric anomaly
43.54507°
Mean motion
3.7736 °/min
Orbital period
95.4 mins
BSTAR
0.00028787
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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 | 2026-11-01 18:46:44.070Z | 352.238° N | 2026-11-01 18:48:44.070Z | 308.761° NW | 44.339° | 2026-11-01 18:52:44.070Z | 213.574° SW |
| 5 mins | 2026-11-02 05:29:44.070Z | 160.596° S | 2026-11-02 05:31:44.070Z | 81.394° E | 80.409° | 2026-11-02 05:34:44.070Z | 350.819° N |
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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