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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Edit Public Description
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 25293.88342028 .00014404 00000-0 13278-2 0 9991
2 64841 97.7580 46.5496 0007436 304.4338 55.6179 14.94766281 18190Epoch: 2025-10-20T21:12Z
TLE epoch observation values (Epoch: 2025-10-20T21:12:07.512Z)
Latitude
-0.00002°
Longitude
58.93896°
Altitude
583.223 km
Speed
7.57 km/s
True Right ascension
03h 06m 11s
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
01:35:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.287 km
Perigee altitude
574.939 km
Semi-major axis
6,958.25 km
Eccentricity
0.00074
Inclination
97.758°
RAAN
46.5496°
Arg. of periapsis
304.4338°
True anomaly
55.68826°
Mean anomaly
55.6179°
Eccentric anomaly
55.65308°
Mean motion
3.73932 °/min
Orbital period
96.27 mins
BSTAR
0.0013278
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-21 06:58:54.068Z | 126.437° SE | 2025-10-21 07:01:54.068Z | 68.963° E | 26.47° | 2025-10-21 07:04:54.068Z | 13.64° NNE |
| 4 mins | 2025-10-21 08:35:54.068Z | 239.803° WSW | 2025-10-21 08:36:54.068Z | 258.766° W | 18.931° | 2025-10-21 08:39:54.068Z | 310.089° NW |
| 6 mins | 2025-10-21 20:16:54.068Z | 28.612° NE | 2025-10-21 20:18:54.068Z | 79.382° E | 39.943° | 2025-10-21 20:22:54.068Z | 179.596° 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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