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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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: 22 hours ago
TLE from 22 hours ago
0 LEMUR 2 MYNAMEISJEFF
1 62712U 25009DH 26287.46566964 .00008663 00000-0 60780-3 0 9992
2 62712 97.7216 10.5194 0003488 129.2571 230.8966 15.05410289 95566Epoch: 2026-10-14T11:10Z
TLE epoch observation values (Epoch: 2026-10-14T11:10:33.856Z)
Latitude
0.00003°
Longitude
179.86334°
Altitude
554.833 km
Speed
7.583 km/s
True Right ascension
00h 42m 04s
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
03:25:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.661 km
Perigee altitude
544.83 km
Semi-major axis
6,925.383 km
Eccentricity
0.00035
Inclination
97.7216°
RAAN
10.5194°
Arg. of periapsis
129.2571°
True anomaly
230.86559°
Mean anomaly
230.8966°
Eccentric anomaly
230.8811°
Mean motion
3.76598 °/min
Orbital period
95.59 mins
BSTAR
0.0006078
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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
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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 | 2026-10-15 18:03:32.296Z | 34.163° NE | 2026-10-15 18:06:32.296Z | 98.819° ESE | 36.99° | 2026-10-15 18:09:32.296Z | 162.462° S |
| 4 mins | 2026-10-16 04:49:32.296Z | 90.664° ESE | 2026-10-16 04:50:32.296Z | 70.096° E | 20.375° | 2026-10-16 04:53:32.296Z | 20.264° NNE |
| 5 mins | 2026-10-16 06:23:32.296Z | 224.486° SW | 2026-10-16 06:25:32.296Z | 273.923° WNW | 27.393° | 2026-10-16 06:28:32.296Z | 323.303° 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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