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: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 KARENDARRELL
1 64841U 25135BU 26260.26527006 .00006514 00000-0 51099-3 0 9996
2 64841 97.7864 16.4860 0010009 259.1174 100.8924 15.01255822 67828Epoch: 2026-09-17T06:21Z
TLE epoch observation values (Epoch: 2026-09-17T06:21:59.333Z)
Latitude
0.00003°
Longitude
-75.21622°
Altitude
567.396 km
Speed
7.577 km/s
True Right ascension
01h 05m 56s
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
06:19:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.975 km
Perigee altitude
553.086 km
Semi-major axis
6,938.167 km
Eccentricity
0.001
Inclination
97.7864°
RAAN
16.486°
Arg. of periapsis
259.1174°
True anomaly
101.005°
Mean anomaly
100.8924°
Eccentric anomaly
100.9487°
Mean motion
3.75557 °/min
Orbital period
95.86 mins
BSTAR
0.00051099
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-17 19:45:08.350Z | 54.615° ENE | 2026-09-17 19:47:08.350Z | 85.865° E | 17.078° | 2026-09-17 19:50:08.350Z | 134.654° SE |
| 6 mins | 2026-09-17 21:20:08.350Z | 343.551° N | 2026-09-17 21:22:08.350Z | 303.389° NW | 32.752° | 2026-09-17 21:26:08.350Z | 224.487° SW |
| 6 mins | 2026-09-18 08:06:08.350Z | 185.495° SSW | 2026-09-18 08:08:08.350Z | 250.491° W | 62.506° | 2026-09-18 08:12:08.350Z | 340.589° N |
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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