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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Edit Public Description
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: 1 day ago
TLE from 1 day ago
0 LEMUR 2 MARHISYAM
1 60536U 24149BW 25312.64658959 .00021152 00000-0 14794-2 0 9993
2 60536 97.7059 30.0933 0003140 140.0459 220.0999 15.05302516 67235Epoch: 2025-11-08T15:31Z
TLE epoch observation values (Epoch: 2025-11-08T15:31:05.340Z)
Latitude
-0.00001°
Longitude
109.24784°
Altitude
555.304 km
Speed
7.583 km/s
True Right ascension
02h 00m 22s
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
18:08:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.75 km
Perigee altitude
545.401 km
Semi-major axis
6,925.713 km
Eccentricity
0.00031
Inclination
97.7059°
RAAN
30.0933°
Arg. of periapsis
140.0459°
True anomaly
220.07673°
Mean anomaly
220.0999°
Eccentric anomaly
220.08831°
Mean motion
3.76571 °/min
Orbital period
95.6 mins
BSTAR
0.0014794
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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 | 2025-11-10 04:22:13.841Z | 102.996° ESE | 2025-11-10 04:24:13.841Z | 67.842° E | 17.339° | 2025-11-10 04:26:13.841Z | 32.486° NE |
| 5 mins | 2025-11-10 05:57:13.841Z | 222.671° SW | 2025-11-10 05:59:13.841Z | 278.096° WNW | 26.668° | 2025-11-10 06:02:13.841Z | 326.364° NNW |
| 4 mins | 2025-11-10 17:34:13.841Z | 57.492° ENE | 2025-11-10 17:36:13.841Z | 109.164° ESE | 25.299° | 2025-11-10 17:38:13.841Z | 148.637° 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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