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: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 MARHISYAM
1 60536U 24149BW 25286.91445035 .00014620 00000-0 10471-2 0 9992
2 60536 97.7075 4.4139 0001999 214.8628 145.2467 15.04498671 63369Epoch: 2025-10-13T21:56Z
TLE epoch observation values (Epoch: 2025-10-13T21:56:48.510Z)
Latitude
-0.00003°
Longitude
12.50138°
Altitude
557.244 km
Speed
7.582 km/s
True Right ascension
00h 17m 39s
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
10:33:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
551.43 km
Perigee altitude
548.66 km
Semi-major axis
6,928.182 km
Eccentricity
0.0002
Inclination
97.7075°
RAAN
4.4139°
Arg. of periapsis
214.8628°
True anomaly
145.25976°
Mean anomaly
145.2467°
Eccentric anomaly
145.25323°
Mean motion
3.76369 °/min
Orbital period
95.65 mins
BSTAR
0.0010471
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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 | 2025-10-14 17:39:51.236Z | 29.635° NE | 2025-10-14 17:43:51.236Z | 112.309° ESE | 30.61° | 2025-10-14 17:46:51.236Z | 165.172° S |
| 4 mins | 2025-10-15 04:26:51.236Z | 91.9° ESE | 2025-10-15 04:27:51.236Z | 71.273° E | 19.447° | 2025-10-15 04:30:51.236Z | 20.511° NNE |
| 5 mins | 2025-10-15 06:00:51.236Z | 223.161° SW | 2025-10-15 06:02:51.236Z | 270.778° WNW | 24.53° | 2025-10-15 06:05:51.236Z | 322.06° 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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