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PADRE

In orbit NORAD 64559 VNWS-4720-9290-9692-1890 United States of America

Time in UTC

12.10 20:51

Scheduled · Сампо-400 [R1NAV]

144

Observations over 30 days

79%

Successful observations

61k

Frames, latest 2026-10-11 22:26 UTC

Mission information
Spacecraft name
PADRE
Other names
PADRE
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2025-06-23 21:25:00
Separation time
2025-06-23 23:41:09
Last observers
Observer
Time of receipt
2026-10-11 22:26:53 UTC
2026-10-11 22:24:27 UTC
2026-10-11 20:53:20 UTC
2026-10-11 20:47:52 UTC
2026-10-11 13:03:44 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
585.52 km
Apogee
586.98 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6964.4 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:36 UTC
Two-line elements (TLE)
1 64559U 25135AH  26284.25233705  .00001929  00000-0  19205-3 0  9995
2 64559 97.7823 36.5023 0001055 189.8392 170.2807 14.92792997 71166
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-12 14:31:28 PADRE
NORAD 64559
KOYO
NORAD 69916
2.981 14.35 2.2e-07
2026-10-13 01:01:19 PADRE
NORAD 64559
COSMOS 2251 DEB
NORAD 37487
4.950 11.71 1.2e-07
2026-10-13 14:14:14 PADRE
NORAD 64559
SPOT 1
NORAD 16613
3.510 14.95 2.7e-06
2026-10-13 16:27:05 PADRE
NORAD 64559
COSMOS 2251 DEB
NORAD 38208
3.978 14.55 1.2e-07
2026-10-13 16:32:08 PERSEUS-M2
NORAD 40037
PADRE
NORAD 64559
3.427 14.74 1.5e-07
2026-10-13 19:31:13 PADRE
NORAD 64559
FENGYUN 1C DEB
NORAD 31768
4.477 0.64 2.2e-07
2026-10-14 18:32:37 PADRE
NORAD 64559
NOAA 16 DEB
NORAD 42427
3.168 14.96 1.6e-07
2026-10-15 00:26:17 PADRE
NORAD 64559
CUBY-2
NORAD 69881
3.239 14.35 1.9e-07
2026-10-15 10:05:24 PADRE
NORAD 64559
RAFS
NORAD 69923
1.131 14.36 1.5e-06
2026-10-15 22:15:42 PADRE
NORAD 64559
ARVAKER-2
NORAD 64567
4.525 0.09 2.2e-07
2026-10-17 01:57:22 OBJECT C
NORAD 51948
PADRE
NORAD 64559
4.565 14.87 7.8e-08
2026-10-17 10:25:46 PADRE
NORAD 64559
UK-DMC
NORAD 27942
2.783 9.55 4.6e-07
2026-10-17 10:30:27 PADRE
NORAD 64559
SL-14 R/B
NORAD 12988
4.599 8.72 4.2e-07
2026-10-17 12:53:20 PADRE
NORAD 64559
CZ-6A DEB
NORAD 54484
3.798 3.77 3.0e-07
2026-10-17 19:01:40 PADRE
NORAD 64559
COSMOS 2251 DEB
NORAD 35898
2.889 3.51 5.2e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite