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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEMUR 2 KARENDARRELL
1 64841U 25135BU 26224.26791350 .00003087 00000-0 24726-3 0 9990
2 64841 97.7776 340.4351 0012950 20.2650 339.9085 15.00840417 62421Epoch: 2026-08-12T06:25Z
TLE epoch observation values (Epoch: 2026-08-12T06:25:47.726Z)
Latitude
-0.00002°
Longitude
-76.73805°
Altitude
558.913 km
Speed
7.587 km/s
True Right ascension
22h 41m 44s
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
21:45:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.298 km
Perigee altitude
552.324 km
Semi-major axis
6,939.448 km
Eccentricity
0.0013
Inclination
97.7776°
RAAN
340.4351°
Arg. of periapsis
20.265°
True anomaly
339.85745°
Mean anomaly
339.9085°
Eccentric anomaly
339.88298°
Mean motion
3.75453 °/min
Orbital period
95.88 mins
BSTAR
0.00024726
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-13 08:09:03.922Z | 185.393° SSW | 2026-08-13 08:12:03.922Z | 241.094° WSW | 37.164° | 2026-08-13 08:16:03.922Z | 336.253° NNW |
| 4 mins | 2026-08-13 19:50:03.922Z | 66.343° ENE | 2026-08-13 19:51:03.922Z | 85.184° E | 18.752° | 2026-08-13 19:54:03.922Z | 138.244° SSE |
| 5 mins | 2026-08-13 21:24:03.922Z | 340.102° N | 2026-08-13 21:26:03.922Z | 301.924° NW | 25.264° | 2026-08-13 21:29:03.922Z | 237.756° WSW |
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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