LEMUR 2 HUBBLE-5, 64840
Orbit data source: Space-Track
LEMUR 2 HUBBLE-5, 64840 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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64840 intel report (Beta)
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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: 14 hours ago
TLE from 14 hours ago
0 LEMUR 2 HUBBLE-5
1 64840U 25135BT 26083.23206222 .00001681 00000-0 16372-3 0 9994
2 64840 97.7607 198.7331 0004276 256.1728 103.9016 14.93840476 41227Epoch: 2026-03-24T05:34Z
TLE epoch observation values (Epoch: 2026-03-24T05:34:10.175Z)
Latitude
-0.00007°
Longitude
-66.52196°
Altitude
589.735 km
Speed
7.565 km/s
True Right ascension
13h 14m 55s
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
00:42:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.967 km
Perigee altitude
580.014 km
Semi-major axis
6,961.127 km
Eccentricity
0.00043
Inclination
97.7607°
RAAN
198.7331°
Arg. of periapsis
256.1728°
True anomaly
103.94916°
Mean anomaly
103.9016°
Eccentric anomaly
103.92538°
Mean motion
3.73701 °/min
Orbital period
96.33 mins
BSTAR
0.00016372
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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-5 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-03-24 20:35:32.899Z | 9.677° NNE | 2026-03-24 20:39:32.899Z | 299.099° NW | 44.439° | 2026-03-24 20:43:32.899Z | 197.865° SSW |
| 6 mins | 2026-03-25 07:25:32.899Z | 150.804° SSE | 2026-03-25 07:28:32.899Z | 64.269° ENE | 41.095° | 2026-03-25 07:31:32.899Z | 357.72° N |
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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