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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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: 12 hours ago
TLE from 12 hours ago
0 LEMUR 2 ROUNDTRIPPER
1 62711U 25009DG 26080.21850176 .00009344 00000-0 71158-3 0 9994
2 62711 97.7285 163.1241 0006121 91.9392 268.2533 15.02281302 64416Epoch: 2026-03-21T05:14Z
TLE epoch observation values (Epoch: 2026-03-21T05:14:38.552Z)
Latitude
-0.00006°
Longitude
-94.27889°
Altitude
563.053 km
Speed
7.58 km/s
True Right ascension
10h 52m 29s
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
22:18:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.112 km
Perigee altitude
552.622 km
Semi-major axis
6,935.004 km
Eccentricity
0.00061
Inclination
97.7285°
RAAN
163.1241°
Arg. of periapsis
91.9392°
True anomaly
268.18319°
Mean anomaly
268.2533°
Eccentric anomaly
268.21825°
Mean motion
3.75814 °/min
Orbital period
95.79 mins
BSTAR
0.00071158
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-21 18:35:27.194Z | 2.885° NNE | 2026-03-21 18:38:27.194Z | 316.885° NNW | 38.96° | 2026-03-21 18:42:27.194Z | 207.348° SW |
| 6 mins | 2026-03-22 05:21:27.194Z | 157.248° SSE | 2026-03-22 05:24:27.194Z | 38.365° NE | 42.789° | 2026-03-22 05:27:27.194Z | 353.03° N |
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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