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: 11 hours ago
TLE from 11 hours ago
0 LEMUR 2 KRISH
1 64561U 25135AK 25328.32232932 .00007513 00000-0 72355-3 0 9995
2 64561 97.7613 80.2608 0001345 96.4226 263.7146 14.93230251 23311Epoch: 2025-11-24T07:44Z
TLE epoch observation values (Epoch: 2025-11-24T07:44:09.253Z)
Latitude
-0.00008°
Longitude
-99.3017°
Altitude
591.018 km
Speed
7.564 km/s
True Right ascension
05h 21m 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
16:09:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.825 km
Perigee altitude
583.952 km
Semi-major axis
6,963.025 km
Eccentricity
0.00013
Inclination
97.7613°
RAAN
80.2608°
Arg. of periapsis
96.4226°
True anomaly
263.69928°
Mean anomaly
263.7146°
Eccentric anomaly
263.70694°
Mean motion
3.73548 °/min
Orbital period
96.37 mins
BSTAR
0.00072355
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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 | 2025-11-24 19:35:18.448Z | 56.825° ENE | 2025-11-24 19:37:18.448Z | 91.498° ESE | 18.712° | 2025-11-24 19:40:18.448Z | 140.188° SSE |
| 5 mins | 2025-11-24 21:11:18.448Z | 329.317° NNW | 2025-11-24 21:13:18.448Z | 278.589° WNW | 26.72° | 2025-11-24 21:16:18.448Z | 229.336° WSW |
| 6 mins | 2025-11-25 07:59:18.448Z | 189.993° SSW | 2025-11-25 08:02:18.448Z | 269.174° W | 37.278° | 2025-11-25 08:05:18.448Z | 332.671° NNW |
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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