LEMUR 2 LIA-MARTIN, 63248
Orbit data source: Space-Track
LEMUR 2 LIA-MARTIN, 63248 is a payload satellite owned by Spire (US) in SSO that was launched on Sat, 15 Mar 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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63248 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEMUR 2 LIA-MARTIN
1 63248U 25052AQ 26284.41857342 .00006477 00000-0 54469-3 0 9998
2 63248 97.6704 175.0137 0003124 141.1255 219.0193 14.98604722 86081Epoch: 2026-10-11T10:02Z
TLE epoch observation values (Epoch: 2026-10-11T10:02:44.743Z)
Latitude
-0.00001°
Longitude
4.31564°
Altitude
575.947 km
Speed
7.572 km/s
True Right ascension
11h 40m 03s
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
21:36:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.382 km
Perigee altitude
566.042 km
Semi-major axis
6,946.349 km
Eccentricity
0.00031
Inclination
97.6704°
RAAN
175.0137°
Arg. of periapsis
141.1255°
True anomaly
218.99677°
Mean anomaly
219.0193°
Eccentric anomaly
219.00803°
Mean motion
3.74894 °/min
Orbital period
96.03 mins
BSTAR
0.00054469
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Other satellites on launch #52 in the year 2025 (2025-03-15 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 LIA-MARTIN 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-12 05:50:35.992Z | 6.775° NNE | 2026-10-12 05:53:35.992Z | 302.58° NW | 72.389° | 2026-10-12 05:57:35.992Z | 200.028° SSW |
| 6 mins | 2026-10-12 16:37:35.992Z | 150.716° SSE | 2026-10-12 16:40:35.992Z | 64.705° ENE | 59.79° | 2026-10-12 16:43:35.992Z | 358.01° 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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