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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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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 LEMUR 2 KRISH
1 64561U 25135AK 26289.55114036 .00004711 00000-0 41281-3 0 9992
2 64561 97.7863 43.7405 0001653 90.0203 270.1208 14.97149577 72076Epoch: 2026-10-16T13:13Z
TLE epoch observation values (Epoch: 2026-10-16T13:13:38.527Z)
Latitude
-0°
Longitude
-179.74056°
Altitude
578.755 km
Speed
7.571 km/s
True Right ascension
02h 54m 57s
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
04:08:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.871 km
Perigee altitude
571.573 km
Semi-major axis
6,950.859 km
Eccentricity
0.00017
Inclination
97.7863°
RAAN
43.7405°
Arg. of periapsis
90.0203°
True anomaly
270.10186°
Mean anomaly
270.1208°
Eccentric anomaly
270.11133°
Mean motion
3.74529 °/min
Orbital period
96.12 mins
BSTAR
0.00041281
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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 | 2026-10-17 20:16:46.624Z | 28.834° NE | 2026-10-17 20:19:46.624Z | 99.92° ESE | 48.519° | 2026-10-17 20:22:46.624Z | 170.43° S |
| 6 mins | 2026-10-18 07:04:46.624Z | 120.678° SE | 2026-10-18 07:06:46.624Z | 83.685° E | 27.793° | 2026-10-18 07:10:46.624Z | 10.672° NNE |
| 4 mins | 2026-10-18 08:40:46.624Z | 232.724° WSW | 2026-10-18 08:42:46.624Z | 271.61° WNW | 20.744° | 2026-10-18 08:44:46.624Z | 306.251° NW |
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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