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: 23 hours ago
TLE from 23 hours ago
0 LEMUR 2 MYNAMEISJEFF
1 62712U 25009DH 25353.16980269 .00008463 00000-0 68263-3 0 9992
2 62712 97.7265 71.8111 0004604 85.6838 274.4911 15.00120844 50601Epoch: 2025-12-19T04:04Z
TLE epoch observation values (Epoch: 2025-12-19T04:04:30.952Z)
Latitude
-0.00006°
Longitude
-77.33267°
Altitude
569.328 km
Speed
7.576 km/s
True Right ascension
04h 47m 14s
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
02:09:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.726 km
Perigee altitude
560.334 km
Semi-major axis
6,941.667 km
Eccentricity
0.00046
Inclination
97.7265°
RAAN
71.8111°
Arg. of periapsis
85.6838°
True anomaly
274.4385°
Mean anomaly
274.4911°
Eccentric anomaly
274.4648°
Mean motion
3.75273 °/min
Orbital period
95.93 mins
BSTAR
0.00068263
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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 | 2025-12-20 05:49:16.885Z | 193.405° SSW | 2025-12-20 05:52:16.885Z | 281.833° WNW | 35.186° | 2025-12-20 05:55:16.885Z | 333.444° NNW |
| 5 mins | 2025-12-20 17:29:16.885Z | 56.126° ENE | 2025-12-20 17:31:16.885Z | 94.629° ESE | 20.52° | 2025-12-20 17:34:16.885Z | 145.383° SSE |
| 5 mins | 2025-12-20 19:04:16.885Z | 332.839° NNW | 2025-12-20 19:06:16.885Z | 290.536° WNW | 23.79° | 2025-12-20 19:09:16.885Z | 236.32° WSW |
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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