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, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 LEMUR 2 KRISH
1 64561U 25135AK 26062.30382632 .00008364 00000-0 76982-3 0 9997
2 64561 97.7611 178.0854 0001028 114.9213 245.2115 14.94993161 38097Epoch: 2026-03-03T07:17Z
TLE epoch observation values (Epoch: 2026-03-03T07:17:30.594Z)
Latitude
0.00006°
Longitude
-92.3769°
Altitude
585.74 km
Speed
7.567 km/s
True Right ascension
11h 52m 20s
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
23:39:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.124 km
Perigee altitude
578.693 km
Semi-major axis
6,957.546 km
Eccentricity
0.0001
Inclination
97.7611°
RAAN
178.0854°
Arg. of periapsis
114.9213°
True anomaly
245.20081°
Mean anomaly
245.2115°
Eccentric anomaly
245.20615°
Mean motion
3.73989 °/min
Orbital period
96.26 mins
BSTAR
0.00076982
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-03 20:42:37.249Z | 4.35° NNE | 2026-03-03 20:45:37.249Z | 299.559° NW | 42.285° | 2026-03-03 20:49:37.249Z | 203.376° SW |
| 6 mins | 2026-03-04 07:31:37.249Z | 155.915° SSE | 2026-03-04 07:33:37.249Z | 124.458° SE | 41.825° | 2026-03-04 07:37:37.249Z | 352.856° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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