LEMUR 2 MARHISYAM, 60536
Orbit data source: Space-Track
LEMUR 2 MARHISYAM, 60536 is a payload satellite owned by Spire (US) in SSO that was launched on Fri, 16 Aug 2024 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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60536 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 LEMUR 2 MARHISYAM
1 60536U 24149BW 26129.44951212 .00009036 00000-0 55290-3 0 9990
2 60536 97.6868 212.1718 0001299 211.0500 149.0652 15.10456780 94634Epoch: 2026-05-09T10:47Z
TLE epoch observation values (Epoch: 2026-05-09T10:47:17.847Z)
Latitude
-0.00006°
Longitude
-176.91934°
Altitude
538.646 km
Speed
7.593 km/s
True Right ascension
14h 08m 41s
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
02:46:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.694 km
Perigee altitude
530.899 km
Semi-major axis
6,909.934 km
Eccentricity
0.00013
Inclination
97.6868°
RAAN
212.1718°
Arg. of periapsis
211.05°
True anomaly
149.07285°
Mean anomaly
149.0652°
Eccentric anomaly
149.06903°
Mean motion
3.77861 °/min
Orbital period
95.27 mins
BSTAR
0.0005529
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Other satellites on launch #149 in the year 2024 (2024-08-16 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 MARHISYAM 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 | 2026-05-09 19:18:28.984Z | 328.219° NNW | 2026-05-09 19:20:28.984Z | 290.6° WNW | 18.405° | 2026-05-09 19:22:28.984Z | 253.81° W |
| 5 mins | 2026-05-10 06:00:28.984Z | 206.919° SW | 2026-05-10 06:02:28.984Z | 263.552° W | 31.682° | 2026-05-10 06:05:28.984Z | 327.571° NNW |
| 4 mins | 2026-05-10 17:35:28.984Z | 60.338° ENE | 2026-05-10 17:37:28.984Z | 102.6° ESE | 20.039° | 2026-05-10 17:39:28.984Z | 139.16° SSE |
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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