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: 14 hours ago
TLE from 14 hours ago
0 LEMUR 2 KARENDARRELL
1 64841U 25135BU 26289.78896826 .00007458 00000-0 57854-3 0 9996
2 64841 97.7905 46.0968 0011166 145.5544 214.6406 15.01623262 72255Epoch: 2026-10-16T18:56Z
TLE epoch observation values (Epoch: 2026-10-16T18:56:06.857Z)
Latitude
-0.00002°
Longitude
96.76329°
Altitude
571.324 km
Speed
7.572 km/s
True Right ascension
03h 04m 23s
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
04:07:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.643 km
Perigee altitude
551.152 km
Semi-major axis
6,937.034 km
Eccentricity
0.00112
Inclination
97.7905°
RAAN
46.0968°
Arg. of periapsis
145.5544°
True anomaly
214.56795°
Mean anomaly
214.6406°
Eccentric anomaly
214.60427°
Mean motion
3.75649 °/min
Orbital period
95.83 mins
BSTAR
0.00057854
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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 | 2026-10-17 21:05:28.831Z | 358.046° N | 2026-10-17 21:08:28.831Z | 278.294° WNW | 52.142° | 2026-10-17 21:11:28.831Z | 212.515° SW |
| 6 mins | 2026-10-18 07:51:28.831Z | 161.534° S | 2026-10-18 07:53:28.831Z | 139.16° SSE | 71.578° | 2026-10-18 07:57:28.831Z | 349.919° N |
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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