RU | EN | ZH --:-- UTC Sign in

SATORO-T3

In orbit NORAD 64589 ERBZ-8933-2960-3678-6096

Time in UTC

—

No observations scheduled

2

Observations over 30 days

58%

Successful observations

7k

Frames, latest 2026-10-09 11:21 UTC

Mission information
Spacecraft name
SATORO-T3
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 23:41:28
Last observers
Observer
Time of receipt
2026-10-09 11:21:44 UTC
2026-10-06 11:05:10 UTC
2026-07-13 21:24:31 UTC
2026-07-06 12:51:59 UTC
2026-07-06 11:16:58 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
577.22 km
Apogee
582.56 km
Inclination
97.8°
Period
96.3 min
Semi-major axis
6958.0 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:50 UTC
Two-line elements (TLE)
1 64589U 25135BP  26283.25082660  .00003288  00000-0  30722-3 0  9996
2 64589 97.7813 36.7000 0003832 317.4425 42.6498 14.94838684 71092
Copy content
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
2026-10-10 21:46:41 SATORO-T3
NORAD 64589
COSMOS 2251 DEB
NORAD 38208
2.868 14.75 2.1e-07
2026-10-11 03:48:12 SATORO-T3
NORAD 64589
INHA-ROSAT
NORAD 66653
4.694 14.97 7.2e-08
2026-10-11 14:39:32 SATORO-T3
NORAD 64589
THORAD AGENA D DEB
NORAD 4938
1.381 8.80 1.9e-06
2026-10-11 21:42:00 SATORO-T3
NORAD 64589
PEGASUS DEB
NORAD 25445
4.818 6.22 1.8e-07
2026-10-12 11:58:41 SATORO-T3
NORAD 64589
NOAA 16 DEB
NORAD 41156
3.661 14.91 1.2e-07
2026-10-13 13:55:29 SATORO-T3
NORAD 64589
CZ-4B DEB
NORAD 26432
3.609 5.29 3.2e-07
2026-10-13 22:57:00 PERSEUS-M2
NORAD 40037
SATORO-T3
NORAD 64589
0.442 14.77 8.9e-06
2026-10-14 05:55:33 ICEYE-X50
NORAD 63255
SATORO-T3
NORAD 64589
2.211 13.89 4.5e-07
2026-10-14 06:00:44 SATORO-T3
NORAD 64589
OBJECT H
NORAD 100962
2.878 2.26 5.3e-07
2026-10-14 11:31:52 SATORO-T3
NORAD 64589
TORGA
NORAD 100802
3.545 14.26 1.6e-07
2026-10-14 23:39:50 SATORO-T3
NORAD 64589
FENGYUN 1C DEB
NORAD 31021
4.650 1.80 2.0e-07
2026-10-15 02:32:19 SATORO-T3
NORAD 64589
NOAA 16 DEB
NORAD 42427
1.875 14.96 4.5e-07
2026-10-15 04:30:10 SATORO-T3
NORAD 64589
OBJECT E
NORAD 100959
1.772 2.26 1.4e-06
2026-10-15 08:10:04 SATORO-T3
NORAD 64589
SL-6 R/B(2)
NORAD 20666
4.262 14.89 2.5e-07
2026-10-15 09:23:51 SATORO-T3
NORAD 64589
AISSAT 2
NORAD 40075
3.566 13.67 1.8e-07
2026-10-15 19:01:53 ZHEDA PIXING 1C
NORAD 37167
SATORO-T3
NORAD 64589
2.123 13.59 5.2e-07
2026-10-16 03:41:18 SATORO-T3
NORAD 64589
TRANSPORTER-17 OBJECT BE
NORAD 69921
4.901 14.32 8.3e-08
2026-10-16 03:48:21 CAPELLA-15 (ACADIA-5)
NORAD 60544
SATORO-T3
NORAD 64589
3.316 5.57 3.8e-07
2026-10-16 17:18:45 FOX-1A (AO-85)
NORAD 40967
SATORO-T3
NORAD 64589
3.638 14.20 1.5e-07
2026-10-17 00:09:44 SATORO-T3
NORAD 64589
ATLAS CENTAUR 2 DEB
NORAD 701
4.128 12.95 1.6e-07
2026-10-17 01:29:29 LEMUR-2-WILSON
NORAD 62694
SATORO-T3
NORAD 64589
4.072 4.76 2.5e-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