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 26192.77535731 .00005347 00000-0 38945-3 0 9993
2 62712 97.7298 275.8188 0003769 105.2846 254.8796 15.04187846 81321Epoch: 2026-07-11T18:36Z
TLE epoch observation values (Epoch: 2026-07-11T18:36:30.871Z)
Latitude
-0.00007°
Longitude
67.00645°
Altitude
557.742 km
Speed
7.582 km/s
True Right ascension
18h 23m 16s
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
15:49:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
553.612 km
Perigee altitude
548.389 km
Semi-major axis
6,929.138 km
Eccentricity
0.00038
Inclination
97.7298°
RAAN
275.8188°
Arg. of periapsis
105.2846°
True anomaly
254.83791°
Mean anomaly
254.8796°
Eccentric anomaly
254.85875°
Mean motion
3.76291 °/min
Orbital period
95.67 mins
BSTAR
0.00038945
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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 | 2026-07-12 05:55:23.670Z | 192.562° SSW | 2026-07-12 05:57:23.670Z | 248.8° W | 37.938° | 2026-07-12 06:01:23.670Z | 337.242° NNW |
| 4 mins | 2026-07-12 17:33:23.670Z | 61.971° ENE | 2026-07-12 17:35:23.670Z | 99.356° ESE | 17.621° | 2026-07-12 17:37:23.670Z | 133.393° SE |
| 4 mins | 2026-07-12 19:08:23.670Z | 328.556° NNW | 2026-07-12 19:10:23.670Z | 276.284° WNW | 25.738° | 2026-07-12 19:12:23.670Z | 237.231° 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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