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SATMAR

In orbit NORAD 64551 XWXT-1615-5633-9630-7970

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

1

Observations all time

Mission information
Spacecraft name
SATMAR
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
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 22:21:17
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
482.62 km
Apogee
484.50 km
Inclination
97.5°
Period
94.3 min
Semi-major axis
6861.6 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 64551U 25135Z   26284.07303113  .00010999  00000-0  42506-3 0  9995
2 64551 97.4729 39.6217 0001426 141.0800 219.0541 15.26415112 72599
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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
2026-10-11 16:30:31 STARLINK-30126
NORAD 56694
SATMAR
NORAD 64551
4.832 11.54 4.0e-06
2026-10-11 17:51:21 TIANMU-1 15
NORAD 58700
SATMAR
NORAD 64551
2.422 8.75 6.3e-07
2026-10-13 00:51:36 STARLINK-2588
NORAD 48398
SATMAR
NORAD 64551
4.260 6.20 6.8e-06
2026-10-13 01:33:27 STARLINK-32630
NORAD 62047
SATMAR
NORAD 64551
4.853 10.30 4.4e-06
2026-10-13 02:19:00 STARLINK-4483
NORAD 53532
SATMAR
NORAD 64551
4.807 13.74 3.0e-06
2026-10-13 03:53:21 STARLINK-4483
NORAD 53532
SATMAR
NORAD 64551
4.682 13.73 3.2e-06
2026-10-13 05:17:37 SVYATOBOR 1 (RS60S)
NORAD 57187
SATMAR
NORAD 64551
4.383 6.49 2.1e-07
2026-10-13 06:14:51 STARLINK-4483
NORAD 53532
SATMAR
NORAD 64551
4.562 13.73 3.4e-06
2026-10-13 14:16:33 KSM1-D
NORAD 46907
SATMAR
NORAD 64551
3.521 7.87 3.1e-07
2026-10-13 18:52:06 STARLINK-5768
NORAD 57145
SATMAR
NORAD 64551
4.958 9.99 4.3e-06
2026-10-14 01:13:09 YAOGAN-36 02A
NORAD 54042
SATMAR
NORAD 64551
1.866 9.27 1.0e-06
2026-10-14 07:26:36 STARLINK-6141
NORAD 57112
SATMAR
NORAD 64551
4.803 10.92 4.3e-06
2026-10-14 12:13:35 STARLINK-32330
NORAD 61850
SATMAR
NORAD 64551
4.983 8.13 4.7e-06
2026-10-15 05:32:00 STARLINK-33613
NORAD 63286
SATMAR
NORAD 64551
4.650 8.10 5.3e-06
2026-10-15 06:12:52 SATMAR
NORAD 64551
DELTA 2 R/B
NORAD 25876
4.934 12.02 1.2e-07
2026-10-15 11:28:50 OTP-2
NORAD 63235
SATMAR
NORAD 64551
2.676 13.97 3.1e-07
2026-10-16 07:04:37 STARLINK-5615
NORAD 55425
SATMAR
NORAD 64551
3.770 14.88 3.6e-06
2026-10-16 09:14:27 YAOGAN-36 01A
NORAD 53943
SATMAR
NORAD 64551
4.784 13.86 9.9e-08
2026-10-16 10:44:59 YAOGAN-35 01C
NORAD 49393
SATMAR
NORAD 64551
4.116 13.94 1.3e-07
2026-10-16 17:46:09 STARLINK-30377
NORAD 57825
SATMAR
NORAD 64551
4.875 7.32 5.0e-06
2026-10-16 19:16:28 STARLINK-30158
NORAD 57438
SATMAR
NORAD 64551
4.552 8.52 5.5e-06
2026-10-17 01:32:07 STARLINK-6111
NORAD 57102
SATMAR
NORAD 64551
4.956 9.76 4.3e-06
2026-10-17 07:49:35 STARLINK-30393
NORAD 57866
SATMAR
NORAD 64551
4.930 9.85 4.4e-06
2026-10-17 08:09:12 SATMAR
NORAD 64551
AVUM R/B
NORAD 40698
4.557 14.98 7.9e-08

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