LEMUR 2 ROUNDTRIPPER, 62711
Orbit data source: Space-Track
LEMUR 2 ROUNDTRIPPER, 62711 is a payload satellite owned by Spire (US) in SSO that was launched on Tue, 14 Jan 2025 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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62711 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, 0.2 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 ROUNDTRIPPER
1 62711U 25009DG 26034.17875269 .00010316 00000-0 80586-3 0 9994
2 62711 97.7279 117.2614 0003287 254.7773 105.3088 15.01295876 57503Epoch: 2026-02-03T04:17Z
TLE epoch observation values (Epoch: 2026-02-03T04:17:24.232Z)
Latitude
0.00001°
Longitude
-80.45298°
Altitude
566.558 km
Speed
7.578 km/s
True Right ascension
07h 49m 02s
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
11:13:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.185 km
Perigee altitude
557.624 km
Semi-major axis
6,938.041 km
Eccentricity
0.00033
Inclination
97.7279°
RAAN
117.2614°
Arg. of periapsis
254.7773°
True anomaly
105.34513°
Mean anomaly
105.3088°
Eccentric anomaly
105.32696°
Mean motion
3.75567 °/min
Orbital period
95.85 mins
BSTAR
0.00080586
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Other satellites on launch #9 in the year 2025 (2025-01-14 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 ROUNDTRIPPER 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 | 2026-02-04 17:39:19.210Z | 38.741° NE | 2026-02-04 17:42:19.210Z | 94° ESE | 25.749° | 2026-02-04 17:45:19.210Z | 152.911° SSE |
| 4 mins | 2026-02-04 19:15:19.210Z | 326.958° NNW | 2026-02-04 19:17:19.210Z | 289.335° WNW | 19.075° | 2026-02-04 19:19:19.210Z | 253.543° W |
| 5 mins | 2026-02-05 06:01:19.210Z | 215.238° SW | 2026-02-05 06:03:19.210Z | 270.694° WNW | 29.417° | 2026-02-05 06:06:19.210Z | 326.048° 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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