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: 11 hours ago
TLE from 11 hours ago
0 LEMUR 2 MYNAMEISJEFF
1 62712U 25009DH 25286.15884726 .00017326 00000-0 14614-2 0 9995
2 62712 97.7301 5.3535 0000406 196.9897 163.1312 14.98215163 40569Epoch: 2025-10-13T03:48Z
TLE epoch observation values (Epoch: 2025-10-13T03:48:44.403Z)
Latitude
0.00001°
Longitude
-73.79715°
Altitude
575.732 km
Speed
7.573 km/s
True Right ascension
00h 21m 24s
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
08:55:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.702 km
Perigee altitude
569.138 km
Semi-major axis
6,947.557 km
Eccentricity
0.00004
Inclination
97.7301°
RAAN
5.3535°
Arg. of periapsis
196.9897°
True anomaly
163.13255°
Mean anomaly
163.1312°
Eccentric anomaly
163.13187°
Mean motion
3.74796 °/min
Orbital period
96.05 mins
BSTAR
0.0014614
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-13 17:13:29.522Z | 56.175° ENE | 2025-10-13 17:15:29.522Z | 86.362° E | 14.983° | 2025-10-13 17:17:29.522Z | 119.924° SE |
| 6 mins | 2025-10-13 18:48:29.522Z | 347.83° N | 2025-10-13 18:51:29.522Z | 275.459° WNW | 30.774° | 2025-10-13 18:54:29.522Z | 222.725° SW |
| 6 mins | 2025-10-14 05:35:29.522Z | 178.966° S | 2025-10-14 05:38:29.522Z | 292.873° NW | 41.866° | 2025-10-14 05:41:29.522Z | 340.725° N |
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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