LIDE, 64869
Orbit data source: Space-Track
LIDE, 64869 is an Italian payload satellite in SSO that was launched on Wed, 23 Jul 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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64869 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
Tyvak Intl
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~15 kg wet, ~15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LIDE
1 64869U 25154A 26269.95235311 .00002022 00000-0 19061-3 0 9990
2 64869 97.6619 331.4631 0003989 244.0903 115.9907 14.94892298 64205Epoch: 2026-09-26T22:51Z
TLE epoch observation values (Epoch: 2026-09-26T22:51:23.308Z)
Latitude
-0.00002°
Longitude
-17.13705°
Altitude
586.974 km
Speed
7.566 km/s
True Right ascension
22h 05m 51s
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
21:47:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.493 km
Perigee altitude
576.942 km
Semi-major axis
6,957.854 km
Eccentricity
0.0004
Inclination
97.6619°
RAAN
331.4631°
Arg. of periapsis
244.0903°
True anomaly
116.03178°
Mean anomaly
115.9907°
Eccentric anomaly
116.01124°
Mean motion
3.73964 °/min
Orbital period
96.27 mins
BSTAR
0.00019061
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Other satellites on launch #154 in the year 2025 (2025-07-23 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.LIDE 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 | 2026-09-28 17:11:39.770Z | 7.996° NNE | 2026-09-28 17:14:39.770Z | 309.212° NW | 75.788° | 2026-09-28 17:18:39.770Z | 198.593° SSW |
| 6 mins | 2026-09-29 04:00:39.770Z | 148.235° SSE | 2026-09-29 04:02:39.770Z | 106.764° ESE | 56.111° | 2026-09-29 04:06:39.770Z | 356.712° 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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