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.
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
63248 intel report (Beta)
Focus sentinelFocus sentinel
Create New Watchlist
Focus sentinelFocus sentinel
Edit Public Description
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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 LIA-MARTIN
1 63248U 25052AQ 25286.98588260 .00009832 00000-0 91991-3 0 9990
2 63248 97.7112 178.3201 0001924 332.9391 27.1729 14.94292144 31866Epoch: 2025-10-13T23:39Z
TLE epoch observation values (Epoch: 2025-10-13T23:39:40.256Z)
Latitude
-0°
Longitude
160.62157°
Altitude
586.425 km
Speed
7.568 km/s
True Right ascension
11h 53m 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
11:57:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.923 km
Perigee altitude
580.245 km
Semi-major axis
6,959.721 km
Eccentricity
0.00019
Inclination
97.7112°
RAAN
178.3201°
Arg. of periapsis
332.9391°
True anomaly
27.18297°
Mean anomaly
27.1729°
Eccentric anomaly
27.17794°
Mean motion
3.73814 °/min
Orbital period
96.3 mins
BSTAR
0.00091991
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #52 in the year 2025 (2025-03-15 UTC)
Did you know?
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
Loading observer location...
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 | 2025-10-14 17:27:21.506Z | 198.069° SSW | 2025-10-14 17:30:21.506Z | 247.498° WSW | 28.813° | 2025-10-14 17:34:21.506Z | 327.43° NNW |
| 6 mins | 2025-10-15 05:10:21.506Z | 40.607° NE | 2025-10-15 05:13:21.506Z | 107.775° ESE | 28.417° | 2025-10-15 05:16:21.506Z | 159.845° S |
| 4 mins | 2025-10-15 06:46:21.506Z | 324.984° NNW | 2025-10-15 06:48:21.506Z | 289.493° WNW | 17.942° | 2025-10-15 06:50:21.506Z | 256.029° W |
| 4 mins | 2025-10-15 16:00:21.506Z | 98.363° ESE | 2025-10-15 16:02:21.506Z | 58.801° ENE | 19.565° | 2025-10-15 16:04:21.506Z | 25.756° NE |
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 ascending order |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
|---|