LEMUR 2 HUBBLE-4, 64565
Orbit data source: Space-Track
LEMUR 2 HUBBLE-4, 64565 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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64565 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 1.4 m
Radar Cross Section
0.326 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LEMUR 2 HUBBLE-4
1 64565U 25135AP 25328.28762015 .00001854 00000-0 18810-3 0 9992
2 64565 97.7566 80.0595 0001548 218.4360 141.6749 14.92075145 23305Epoch: 2025-11-24T06:54Z
TLE epoch observation values (Epoch: 2025-11-24T06:54:10.380Z)
Latitude
-0.00004°
Longitude
-86.9735°
Altitude
595.355 km
Speed
7.562 km/s
True Right ascension
05h 20m 14s
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
15:54:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.563 km
Perigee altitude
587.406 km
Semi-major axis
6,966.621 km
Eccentricity
0.00015
Inclination
97.7566°
RAAN
80.0595°
Arg. of periapsis
218.436°
True anomaly
141.6859°
Mean anomaly
141.6749°
Eccentric anomaly
141.6804°
Mean motion
3.73259 °/min
Orbital period
96.45 mins
BSTAR
0.0001881
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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 HUBBLE-4 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 | 2025-11-24 20:21:00.366Z | 18.556° NNE | 2025-11-24 20:24:00.366Z | 71.532° E | 42.982° | 2025-11-24 20:28:00.366Z | 185.728° SSW |
| 6 mins | 2025-11-25 07:11:00.366Z | 137.685° SSE | 2025-11-25 07:14:00.366Z | 66.917° ENE | 34.164° | 2025-11-25 07:17:00.366Z | 5.891° NNE |
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 |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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