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: 8 hours ago
TLE from 8 hours ago
0 LEMUR 2 KARENDARRELL
1 64841U 25135BU 26120.28082816 .00008816 00000-0 72292-3 0 9993
2 64841 97.7690 236.5949 0009070 35.9201 324.2630 14.99452361 46832Epoch: 2026-04-30T06:44Z
TLE epoch observation values (Epoch: 2026-04-30T06:44:23.553Z)
Latitude
0°
Longitude
-82.73293°
Altitude
566.526 km
Speed
7.581 km/s
True Right ascension
15h 46m 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
22:23:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.894 km
Perigee altitude
559.298 km
Semi-major axis
6,943.733 km
Eccentricity
0.00091
Inclination
97.769°
RAAN
236.5949°
Arg. of periapsis
35.9201°
True anomaly
324.20224°
Mean anomaly
324.263°
Eccentric anomaly
324.23263°
Mean motion
3.75106 °/min
Orbital period
95.97 mins
BSTAR
0.00072292
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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 | 2026-04-30 20:07:24.967Z | 32.325° NE | 2026-04-30 20:10:24.967Z | 90.229° ESE | 31.664° | 2026-04-30 20:13:24.967Z | 161.003° S |
| 4 mins | 2026-05-01 06:55:24.967Z | 105.966° ESE | 2026-05-01 06:57:24.967Z | 65.747° ENE | 20.942° | 2026-05-01 06:59:24.967Z | 27.932° NE |
| 5 mins | 2026-05-01 08:30:24.967Z | 224.318° SW | 2026-05-01 08:32:24.967Z | 268.415° W | 23.235° | 2026-05-01 08:35:24.967Z | 319.695° NNW |
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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