LEMUR 2 MYNAMEISJEFF, 62712
Orbit data source: Space-Track
LEMUR 2 MYNAMEISJEFF, 62712 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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62712 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: 10 hours ago
TLE from 10 hours ago
0 LEMUR 2 MYNAMEISJEFF
1 62712U 25009DH 26034.17727733 .00011700 00000-0 91279-3 0 9996
2 62712 97.7338 117.5582 0003537 299.2273 60.8597 15.01308847 57507Epoch: 2026-02-03T04:15Z
TLE epoch observation values (Epoch: 2026-02-03T04:15:16.761Z)
Latitude
-0.00002°
Longitude
-79.62359°
Altitude
564.72 km
Speed
7.579 km/s
True Right ascension
07h 50m 13s
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
16:30:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.318 km
Perigee altitude
557.41 km
Semi-major axis
6,938.001 km
Eccentricity
0.00035
Inclination
97.7338°
RAAN
117.5582°
Arg. of periapsis
299.2273°
True anomaly
60.89511°
Mean anomaly
60.8597°
Eccentric anomaly
60.8774°
Mean motion
3.75571 °/min
Orbital period
95.85 mins
BSTAR
0.00091279
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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 MYNAMEISJEFF Visibility forecast
Loading observer location...
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 | 2026-02-03 17:37:24.732Z | 38.835° NE | 2026-02-03 17:40:24.732Z | 89.628° E | 24.138° | 2026-02-03 17:43:24.732Z | 148.959° SSE |
| 4 mins | 2026-02-03 19:14:24.732Z | 314.24° NW | 2026-02-03 19:15:24.732Z | 293.021° NW | 20.346° | 2026-02-03 19:18:24.732Z | 242.359° WSW |
| 5 mins | 2026-02-04 05:59:24.732Z | 209.641° SW | 2026-02-04 06:01:24.732Z | 265.031° W | 31.276° | 2026-02-04 06:04:24.732Z | 326.485° 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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