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: 10 hours ago
TLE from 10 hours ago
0 LEMUR 2 KRISH
1 64561U 25135AK 26120.11591753 .00005893 00000-0 53378-3 0 9995
2 64561 97.7677 235.3594 0001219 110.7791 249.3560 14.95751124 46735Epoch: 2026-04-30T02:46Z
TLE epoch observation values (Epoch: 2026-04-30T02:46:55.274Z)
Latitude
-0.00009°
Longitude
-24.43805°
Altitude
583.388 km
Speed
7.569 km/s
True Right ascension
15h 41m 26s
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
19:57:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.904 km
Perigee altitude
576.208 km
Semi-major axis
6,955.193 km
Eccentricity
0.00012
Inclination
97.7677°
RAAN
235.3594°
Arg. of periapsis
110.7791°
True anomaly
249.34293°
Mean anomaly
249.356°
Eccentric anomaly
249.34946°
Mean motion
3.74179 °/min
Orbital period
96.21 mins
BSTAR
0.00053378
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-30 19:25:50.286Z | 59.147° ENE | 2026-04-30 19:27:50.286Z | 88.972° E | 14.021° | 2026-04-30 19:29:50.286Z | 120.422° SE |
| 6 mins | 2026-04-30 21:00:50.286Z | 350.274° N | 2026-04-30 21:03:50.286Z | 274.776° WNW | 32.959° | 2026-04-30 21:06:50.286Z | 220.108° SW |
| 6 mins | 2026-05-01 07:48:50.286Z | 176.171° S | 2026-05-01 07:51:50.286Z | 291.39° WNW | 43.042° | 2026-05-01 07:54:50.286Z | 341.873° N |
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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