LEMUR 2 KRISH, 64561
Orbit data source: Space-Track
LEMUR 2 KRISH, 64561 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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64561 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 1.0 m
Radar Cross Section
0.326 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEMUR 2 KRISH
1 64561U 25135AK 25269.26345324 .00012188 00000-0 12054-2 0 9995
2 64561 97.7568 22.0475 0001028 110.2717 249.8612 14.92031713 14509Epoch: 2025-09-26T06:19Z
TLE epoch observation values (Epoch: 2025-09-26T06:19:22.359Z)
Latitude
-0.0001°
Longitude
-78.10838°
Altitude
594.89 km
Speed
7.562 km/s
True Right ascension
01h 28m 11s
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
17:09:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.336 km
Perigee altitude
587.904 km
Semi-major axis
6,966.757 km
Eccentricity
0.0001
Inclination
97.7568°
RAAN
22.0475°
Arg. of periapsis
110.2717°
True anomaly
249.85014°
Mean anomaly
249.8612°
Eccentric anomaly
249.85567°
Mean motion
3.73248 °/min
Orbital period
96.45 mins
BSTAR
0.0012054
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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 KRISH 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 | 2025-09-27 06:37:19.704Z | 105.492° ESE | 2025-09-27 06:39:19.704Z | 74.317° E | 17.219° | 2025-09-27 06:42:19.704Z | 25.856° NE |
| 6 mins | 2025-09-27 08:12:19.704Z | 204.224° SW | 2025-09-27 08:15:19.704Z | 273.31° WNW | 29.587° | 2025-09-27 08:18:19.704Z | 326.086° NNW |
| 5 mins | 2025-09-27 19:56:19.704Z | 49.857° ENE | 2025-09-27 19:58:19.704Z | 99.873° ESE | 29.028° | 2025-09-27 20:01:19.704Z | 158.106° S |
| 4 mins | 2025-09-27 21:32:19.704Z | 315.489° NNW | 2025-09-27 21:33:19.704Z | 297.187° NW | 17.916° | 2025-09-27 21:36:19.704Z | 249.287° W |
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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