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 Com/MetRO
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, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 KRISH
1 64561U 25135AK 25312.10421368 .00009431 00000-0 91443-3 0 9997
2 64561 97.7608 64.2604 0001100 105.9683 254.1657 14.92891139 20893Epoch: 2025-11-08T02:30Z
TLE epoch observation values (Epoch: 2025-11-08T02:30:04.061Z)
Latitude
-0.00011°
Longitude
-20.79512°
Altitude
592.179 km
Speed
7.564 km/s
True Right ascension
04h 17m 02s
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
05:41:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.71 km
Perigee altitude
585.178 km
Semi-major axis
6,964.081 km
Eccentricity
0.00011
Inclination
97.7608°
RAAN
64.2604°
Arg. of periapsis
105.9683°
True anomaly
254.15357°
Mean anomaly
254.1657°
Eccentric anomaly
254.15964°
Mean motion
3.73463 °/min
Orbital period
96.4 mins
BSTAR
0.00091443
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-08 20:46:18.736Z | 358.905° N | 2025-11-08 20:49:18.736Z | 260.431° W | 39.648° | 2025-11-08 20:52:18.736Z | 208.674° SW |
| 6 mins | 2025-11-09 07:35:18.736Z | 163.066° S | 2025-11-09 07:38:18.736Z | 35.793° NE | 44.65° | 2025-11-09 07:41:18.736Z | 349.811° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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