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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEMUR 2 MARHISYAM
1 60536U 24149BW 26236.16670656 .00009154 00000-0 53074-3 0 9997
2 60536 97.6858 319.4841 0001021 177.1015 183.0222 15.12404357110755Epoch: 2026-08-24T04:00Z
TLE epoch observation values (Epoch: 2026-08-24T04:00:03.446Z)
Latitude
0.00003°
Longitude
-72.98257°
Altitude
532.646 km
Speed
7.596 km/s
True Right ascension
21h 17m 56s
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
00:25:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.563 km
Perigee altitude
525.153 km
Semi-major axis
6,903.995 km
Eccentricity
0.0001
Inclination
97.6858°
RAAN
319.4841°
Arg. of periapsis
177.1015°
True anomaly
183.02158°
Mean anomaly
183.0222°
Eccentric anomaly
183.02189°
Mean motion
3.78349 °/min
Orbital period
95.15 mins
BSTAR
0.00053074
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-25 18:40:05.066Z | 6.354° NNE | 2026-08-25 18:43:05.066Z | 320.296° NNW | 42.13° | 2026-08-25 18:47:05.066Z | 201.392° SSW |
| 5 mins | 2026-08-26 05:22:05.066Z | 142.103° SSE | 2026-08-26 05:24:05.066Z | 90.671° ESE | 37.314° | 2026-08-26 05:27:05.066Z | 2.909° NNE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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