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LEMUR 2 EMERSONROSE, 63261

Orbit data source: Space-Track

LEMUR 2 EMERSONROSE, 63261 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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Identifier
63261, 2025-052BD
Orbit
SSO
Country
Flag of USUS
Related 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)
2025-03-15 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 22 hours ago

TLE from 22 hours ago
0 LEMUR 2 EMERSONROSE
1 63261U 25052BD  26074.22156790  .00006606  00000-0  55982-3 0  9993
2 63261  97.7005 328.7802 0001996  32.3684 327.7661 14.98303476 54667
Epoch: 2026-03-15T05:19Z
TLE epoch observation values (Epoch: 2026-03-15T05:19:03.466Z)
Latitude
0.00001°
Longitude
76.18425°
Altitude
574.017 km
Speed
7.574 km/s
True Right ascension
21h 55m 07s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:26:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.532 km
Perigee altitude
567.759 km
Semi-major axis
6,947.282 km
Eccentricity
0.0002
Inclination
97.7005°
RAAN
328.7802°
Arg. of periapsis
32.3684°
True anomaly
327.7539°
Mean anomaly
327.7661°
Eccentric anomaly
327.76°
Mean motion
3.74818 °/min
Orbital period
96.05 mins
BSTAR
0.00055982
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