TIME FLIES, 64564
Orbit data source: Space-Track
TIME FLIES, 64564 is a payload satellite owned by TrustPoint (US) 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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64564 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
TrustPoint
Mission
Operational Commercial Navigation
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 TIME FLIES
1 64564U 25135AN 26178.29642729 .00002837 00000-0 26486-3 0 9995
2 64564 97.7719 292.6620 0001220 201.3855 158.7315 14.94985307 55418Epoch: 2026-06-27T07:06Z
TLE epoch observation values (Epoch: 2026-06-27T07:06:51.317Z)
Latitude
-0.00002°
Longitude
-89.46443°
Altitude
586.256 km
Speed
7.567 km/s
True Right ascension
19h 30m 38s
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
04:19:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.282 km
Perigee altitude
578.585 km
Semi-major axis
6,957.571 km
Eccentricity
0.00012
Inclination
97.7719°
RAAN
292.662°
Arg. of periapsis
201.3855°
True anomaly
158.73657°
Mean anomaly
158.7315°
Eccentric anomaly
158.73404°
Mean motion
3.73987 °/min
Orbital period
96.26 mins
BSTAR
0.00026486
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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.TIME FLIES 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 | 2026-06-27 20:31:26.139Z | 12.557° NNE | 2026-06-27 20:35:26.139Z | 186.536° SSW | 44.753° | 2026-06-27 20:38:26.139Z | 193.086° SSW |
| 6 mins | 2026-06-28 07:21:26.139Z | 139.397° SSE | 2026-06-28 07:23:26.139Z | 83.842° E | 37.945° | 2026-06-28 07:27:26.139Z | 358.567° 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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