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: 16 hours ago
TLE from 16 hours ago
0 LEMUR 2 KARENDARRELL
1 64841U 25135BU 26171.31990221 .00006327 00000-0 51100-3 0 9991
2 64841 97.7680 287.5224 0009932 189.9900 170.1127 15.00147337 54482Epoch: 2026-06-20T07:40Z
TLE epoch observation values (Epoch: 2026-06-20T07:40:39.550Z)
Latitude
-0.0001°
Longitude
-96.1786°
Altitude
576.291 km
Speed
7.569 km/s
True Right ascension
19h 10m 05s
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
10:18:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.344 km
Perigee altitude
556.555 km
Semi-major axis
6,941.587 km
Eccentricity
0.00099
Inclination
97.768°
RAAN
287.5224°
Arg. of periapsis
189.99°
True anomaly
170.13222°
Mean anomaly
170.1127°
Eccentric anomaly
170.12246°
Mean motion
3.7528 °/min
Orbital period
95.93 mins
BSTAR
0.000511
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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 | 2026-06-21 07:48:20.316Z | 168.081° S | 2026-06-21 07:52:20.316Z | 322.048° NNW | 44.585° | 2026-06-21 07:55:20.316Z | 346.222° N |
| 6 mins | 2026-06-21 21:04:20.316Z | 350.289° N | 2026-06-21 21:06:20.316Z | 305.294° NW | 34.319° | 2026-06-21 21:10:20.316Z | 215.304° SW |
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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