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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Edit Public Description
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: 10 hours ago
TLE from 10 hours ago
0 LEMUR 2 KARENDARRELL
1 64841U 25135BU 25340.85601167 .00018251 00000-0 16236-2 0 9994
2 64841 97.7591 93.0450 0008821 141.6489 218.5361 14.96100393 25218Epoch: 2025-12-06T20:32Z
TLE epoch observation values (Epoch: 2025-12-06T20:32:39.408Z)
Latitude
0.00001°
Longitude
69.00305°
Altitude
586.81 km
Speed
7.564 km/s
True Right ascension
06h 12m 10s
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
04:09:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.107 km
Perigee altitude
569.838 km
Semi-major axis
6,954.109 km
Eccentricity
0.00088
Inclination
97.7591°
RAAN
93.045°
Arg. of periapsis
141.6489°
True anomaly
218.47318°
Mean anomaly
218.5361°
Eccentric anomaly
218.50463°
Mean motion
3.74266 °/min
Orbital period
96.19 mins
BSTAR
0.0016236
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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 | 2025-12-07 07:55:22.028Z | 188.089° SSW | 2025-12-07 07:57:22.028Z | 253.164° W | 40.831° | 2025-12-07 08:01:22.028Z | 339.717° N |
| 4 mins | 2025-12-07 19:37:22.028Z | 68.498° E | 2025-12-07 19:38:22.028Z | 86.998° E | 17.937° | 2025-12-07 19:41:22.028Z | 137.599° SSE |
| 5 mins | 2025-12-07 21:12:22.028Z | 330.553° NNW | 2025-12-07 21:14:22.028Z | 279.649° WNW | 26.692° | 2025-12-07 21:17:22.028Z | 229.102° 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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