LEMUR-2-LUCILLE-ROSE, 65403
Orbit data source: Space-Track
LEMUR-2-LUCILLE-ROSE, 65403 is an American payload satellite in SSO that was launched on Mon, 23 Jun 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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65403 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 4U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 14.5 m
Radar Cross Section
0.045 m²
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 LEMUR-2-LUCILLE-ROSE
1 65403U 25135BV 26062.31201071 .00014900 00000-0 12567-2 0 9992
2 65403 97.7601 178.8452 0010200 264.3770 95.6289 14.98213167 32777Epoch: 2026-03-03T07:29Z
TLE epoch observation values (Epoch: 2026-03-03T07:29:17.725Z)
Latitude
-0.00003°
Longitude
-94.57153°
Altitude
576.17 km
Speed
7.572 km/s
True Right ascension
11h 55m 22s
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
01:59:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.514 km
Perigee altitude
562.341 km
Semi-major axis
6,947.565 km
Eccentricity
0.00102
Inclination
97.7601°
RAAN
178.8452°
Arg. of periapsis
264.377°
True anomaly
95.74521°
Mean anomaly
95.6289°
Eccentric anomaly
95.68705°
Mean motion
3.74795 °/min
Orbital period
96.05 mins
BSTAR
0.0012567
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-LUCILLE-ROSE 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 | 2026-03-04 07:39:01.715Z | 163.963° S | 2026-03-04 07:43:01.715Z | 8.207° NNE | 43.824° | 2026-03-04 07:46:01.715Z | 349.435° N |
| 6 mins | 2026-03-04 20:56:01.715Z | 352.082° N | 2026-03-04 20:58:01.715Z | 302.677° NW | 36.93° | 2026-03-04 21:02:01.715Z | 212.035° SW |
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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