LEMUR 2 STELLA, 60533
Orbit data source: Space-Track
LEMUR 2 STELLA, 60533 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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60533 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: 5 days ago
TLE from 5 days ago
0 LEMUR 2 STELLA
1 60533U 24149BT 26154.77678173 .00013306 00000-0 78877-3 0 9994
2 60533 97.6744 237.1777 0001930 107.4795 252.6646 15.11502384 98475Epoch: 2026-06-03T18:38Z
TLE epoch observation values (Epoch: 2026-06-03T18:38:33.941Z)
Latitude
-0°
Longitude
65.30574°
Altitude
535.086 km
Speed
7.595 km/s
True Right ascension
15h 48m 42s
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
04:09:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.939 km
Perigee altitude
527.273 km
Semi-major axis
6,906.743 km
Eccentricity
0.00019
Inclination
97.6744°
RAAN
237.1777°
Arg. of periapsis
107.4795°
True anomaly
252.64349°
Mean anomaly
252.6646°
Eccentric anomaly
252.65404°
Mean motion
3.78123 °/min
Orbital period
95.21 mins
BSTAR
0.00078877
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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 STELLA 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-08 18:21:52.972Z | 13.511° NNE | 2026-06-08 18:24:52.972Z | 79.298° E | 44.926° | 2026-06-08 18:27:52.972Z | 191.598° SSW |
| 5 mins | 2026-06-09 05:03:52.972Z | 131.723° SE | 2026-06-09 05:05:52.972Z | 86.79° E | 30.953° | 2026-06-09 05:08:52.972Z | 10.613° 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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