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, 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 26131.95323245 .00004570 00000-0 34231-3 0 9992
2 62712 97.7299 215.0645 0000789 1.5280 358.5948 15.03202850 72182Epoch: 2026-05-11T22:52Z
TLE epoch observation values (Epoch: 2026-05-11T22:52:39.283Z)
Latitude
0.00003°
Longitude
2.16625°
Altitude
559.539 km
Speed
7.582 km/s
True Right ascension
14h 20m 15s
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
17:40:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
554.577 km
Perigee altitude
553.483 km
Semi-major axis
6,932.167 km
Eccentricity
0.00008
Inclination
97.7299°
RAAN
215.0645°
Arg. of periapsis
1.528°
True anomaly
358.59458°
Mean anomaly
358.5948°
Eccentric anomaly
358.59469°
Mean motion
3.76045 °/min
Orbital period
95.73 mins
BSTAR
0.00034231
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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 | 2026-05-12 18:36:49.248Z | 3.543° NNE | 2026-05-12 18:39:49.248Z | 293.839° NW | 41.768° | 2026-05-12 18:42:49.248Z | 206.79° SW |
| 5 mins | 2026-05-13 05:22:49.248Z | 149.128° SSE | 2026-05-13 05:24:49.248Z | 67.451° ENE | 42.235° | 2026-05-13 05:27:49.248Z | 355.822° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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