LEMUR 2 DELOITTE-1, 63259
Orbit data source: Space-Track
LEMUR 2 DELOITTE-1, 63259 is an American payload satellite 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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63259 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 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: 17 hours ago
TLE from 17 hours ago
0 LEMUR 2 DELOITTE-1
1 63259U 25052BB 25359.64566211 .00006678 00000-0 60294-3 0 9995
2 63259 97.7102 250.0388 0001729 37.0256 323.1084 14.95819248 42739Epoch: 2025-12-25T15:29Z
TLE epoch observation values (Epoch: 2025-12-25T15:29:45.206Z)
Latitude
-0.00003°
Longitude
-76.79728°
Altitude
581.917 km
Speed
7.57 km/s
True Right ascension
16h 40m 09s
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
07:56:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.045 km
Perigee altitude
575.64 km
Semi-major axis
6,954.979 km
Eccentricity
0.00017
Inclination
97.7102°
RAAN
250.0388°
Arg. of periapsis
37.0256°
True anomaly
323.0965°
Mean anomaly
323.1084°
Eccentric anomaly
323.10245°
Mean motion
3.74196 °/min
Orbital period
96.21 mins
BSTAR
0.00060294
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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 DELOITTE-1 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 | 2025-12-26 15:44:39.870Z | 94.927° ESE | 2025-12-26 15:46:39.870Z | 64.175° ENE | 13.957° | 2025-12-26 15:48:39.870Z | 34.058° NE |
| 6 mins | 2025-12-26 17:18:39.870Z | 193.608° SSW | 2025-12-26 17:21:39.870Z | 267.771° W | 34.999° | 2025-12-26 17:24:39.870Z | 330.342° NNW |
| 5 mins | 2025-12-27 05:00:39.870Z | 50.1° ENE | 2025-12-27 05:02:39.870Z | 87.61° E | 22.865° | 2025-12-27 05:05:39.870Z | 145.337° SSE |
| 4 mins | 2025-12-27 06:36:39.870Z | 323.417° NNW | 2025-12-27 06:38:39.870Z | 280.081° WNW | 21.702° | 2025-12-27 06:40:39.870Z | 245.322° WSW |
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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