LEMUR 2 KARENDARRELL, 64841
Orbit data source: Space-Track
LEMUR 2 KARENDARRELL, 64841 is an American payload satellite in SSO that was launched on Mon, 23 Jun 2025 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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64841 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 4U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.045 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 LEMUR 2 KARENDARRELL
1 64841U 25135BU 26062.53685013 .00013890 00000-0 11698-2 0 9994
2 64841 97.7593 179.0952 0007665 203.0704 157.0175 14.98305203 38189Epoch: 2026-03-03T12:53Z
TLE epoch observation values (Epoch: 2026-03-03T12:53:03.851Z)
Latitude
-0.00003°
Longitude
-175.48534°
Altitude
580.089 km
Speed
7.568 km/s
True Right ascension
11h 56m 22s
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
02:02:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.468 km
Perigee altitude
563.818 km
Semi-major axis
6,947.28 km
Eccentricity
0.00077
Inclination
97.7593°
RAAN
179.0952°
Arg. of periapsis
203.0704°
True anomaly
157.05176°
Mean anomaly
157.0175°
Eccentric anomaly
157.03464°
Mean motion
3.74818 °/min
Orbital period
96.05 mins
BSTAR
0.0011698
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Other satellites on launch #135 in the year 2025 (2025-06-23 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 KARENDARRELL 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 | 2026-03-04 06:40:54.442Z | 96.807° ESE | 2026-03-04 06:42:54.442Z | 62.373° ENE | 16.47° | 2026-03-04 06:44:54.442Z | 30.494° NE |
| 6 mins | 2026-03-04 08:14:54.442Z | 202.945° SW | 2026-03-04 08:17:54.442Z | 274.845° WNW | 30.042° | 2026-03-04 08:20:54.442Z | 327.299° NNW |
| 5 mins | 2026-03-04 19:55:54.442Z | 51.653° ENE | 2026-03-04 19:57:54.442Z | 97.207° ESE | 25.868° | 2026-03-04 20:00:54.442Z | 153.843° SSE |
| 4 mins | 2026-03-04 21:30:54.442Z | 328.014° NNW | 2026-03-04 21:32:54.442Z | 290.961° WNW | 19.268° | 2026-03-04 21:34:54.442Z | 254.618° W |
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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