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: 9 hours ago
TLE from 9 hours ago
0 LEMUR 2 ROUNDTRIPPER
1 62711U 25009DG 25286.22695523 .00015557 00000-0 13117-2 0 9998
2 62711 97.7233 5.2105 0001957 189.0067 171.1121 14.98255419 40574Epoch: 2025-10-13T05:26Z
TLE epoch observation values (Epoch: 2025-10-13T05:26:48.931Z)
Latitude
-0.00001°
Longitude
-98.52614°
Altitude
576.682 km
Speed
7.572 km/s
True Right ascension
00h 20m 50s
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
08:55:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.655 km
Perigee altitude
567.936 km
Semi-major axis
6,947.432 km
Eccentricity
0.0002
Inclination
97.7233°
RAAN
5.2105°
Arg. of periapsis
189.0067°
True anomaly
171.11556°
Mean anomaly
171.1121°
Eccentric anomaly
171.11383°
Mean motion
3.74806 °/min
Orbital period
96.05 mins
BSTAR
0.0013117
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-13 17:15:29.063Z | 56.771° ENE | 2025-10-13 17:17:29.063Z | 88.575° E | 16.05° | 2025-10-13 17:19:29.063Z | 123.012° SE |
| 6 mins | 2025-10-13 18:50:29.063Z | 344.705° N | 2025-10-13 18:53:29.063Z | 272.019° WNW | 28.835° | 2025-10-13 18:56:29.063Z | 223.973° SW |
| 7 mins | 2025-10-14 05:36:29.063Z | 178.759° S | 2025-10-14 05:40:29.063Z | 296.717° NW | 39.887° | 2025-10-14 05:43:29.063Z | 339.439° N |
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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