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, 0.2 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 LEMUR 2 MYNAMEISJEFF
1 62712U 25009DH 26238.46751249 .00006433 00000-0 46043-3 0 9999
2 62712 97.7256 321.5059 0001303 326.6999 33.4144 15.04768591 88193Epoch: 2026-08-26T11:13Z
TLE epoch observation values (Epoch: 2026-08-26T11:13:13.079Z)
Latitude
-0.00008°
Longitude
178.48133°
Altitude
554.523 km
Speed
7.585 km/s
True Right ascension
21h 26m 01s
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
11:20:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.119 km
Perigee altitude
548.314 km
Semi-major axis
6,927.353 km
Eccentricity
0.00013
Inclination
97.7256°
RAAN
321.5059°
Arg. of periapsis
326.6999°
True anomaly
33.42262°
Mean anomaly
33.4144°
Eccentric anomaly
33.41851°
Mean motion
3.76437 °/min
Orbital period
95.63 mins
BSTAR
0.00046043
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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 | 2026-08-27 04:54:46.698Z | 125.216° SE | 2026-08-27 04:57:46.698Z | 72.146° E | 23.751° | 2026-08-27 05:00:46.698Z | 16.244° NNE |
| 4 mins | 2026-08-27 06:30:46.698Z | 229.603° WSW | 2026-08-27 06:32:46.698Z | 269.608° W | 19.81° | 2026-08-27 06:34:46.698Z | 306.285° NW |
| 5 mins | 2026-08-27 18:07:46.698Z | 37.885° NE | 2026-08-27 18:09:46.698Z | 92.779° ESE | 34.827° | 2026-08-27 18:12:46.698Z | 167.274° S |
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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