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: 12 hours ago
TLE from 12 hours ago
0 LEMUR 2 MARHISYAM
1 60536U 24149BW 26081.20530755 .00014158 00000-0 89050-3 0 9998
2 60536 97.6894 163.7628 0003255 82.5620 277.5978 15.09324160 87355Epoch: 2026-03-22T04:55Z
TLE epoch observation values (Epoch: 2026-03-22T04:55:38.572Z)
Latitude
-0.00004°
Longitude
-89.86292°
Altitude
541.035 km
Speed
7.592 km/s
True Right ascension
10h 55m 03s
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
22:00:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
537.507 km
Perigee altitude
533.006 km
Semi-major axis
6,913.393 km
Eccentricity
0.00033
Inclination
97.6894°
RAAN
163.7628°
Arg. of periapsis
82.562°
True anomaly
277.56083°
Mean anomaly
277.5978°
Eccentric anomaly
277.57931°
Mean motion
3.77578 °/min
Orbital period
95.34 mins
BSTAR
0.0008905
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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 | 2026-03-22 18:12:51.612Z | 16.106° NNE | 2026-03-22 18:16:51.612Z | 156.956° SSE | 42.263° | 2026-03-22 18:19:51.612Z | 187.403° SSW |
| 5 mins | 2026-03-23 04:56:51.612Z | 121.859° SE | 2026-03-23 04:58:51.612Z | 67.328° ENE | 29.511° | 2026-03-23 05:01:51.612Z | 8.794° 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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