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IPoS-TDsM

In orbit NORAD 69913 QYDP-8943-6593-0386-9661 United States of America

Observations 21
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2026

Falcon 9 Block 5 | Transporter 17 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

21

Observations all time

Mission information
Spacecraft name
IPoS-TDsM
Call sign
WQ2XKO
Website
https://apolink.space/
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Transporter 17 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-07-07 07:12:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
589.82 km
Apogee
593.38 km
Inclination
97.7°
Period
96.6 min
Semi-major axis
6969.7 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:57:00 UTC
Two-line elements (TLE)
1 69913U 26156AW  26283.57330904  .00001117  00000-0  11832-3 0  9998
2 69913  97.7481 182.3525 0002576 163.6955 196.4347 14.91075531 14192
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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 09:29:15 ICEYE-X78
NORAD 68995 		IPOS-TDSM
NORAD 69913 		4.796 0.47 1.9e-07
2026-10-11 15:52:11 IPOS-TDSM
NORAD 69913 		FENGYUN 1C DEB
NORAD 31087 		4.822 13.03 1.1e-07
2026-10-12 08:19:59 IPOS-TDSM
NORAD 69913 		CBERS 1 DEB
NORAD 35387 		0.783 14.95 2.6e-06
2026-10-12 09:56:35 IPOS-TDSM
NORAD 69913 		CBERS 1 DEB
NORAD 35387 		4.428 14.95 8.2e-08
2026-10-12 13:19:14 FIREFLY-3
NORAD 62710 		IPOS-TDSM
NORAD 69913 		2.126 14.98 3.5e-07
2026-10-12 18:36:39 IRIDE-MS2-HEO-9
NORAD 64585 		IPOS-TDSM
NORAD 69913 		3.346 14.29 1.8e-07
2026-10-12 19:24:58 IRIDE-MS2-HEO-9
NORAD 64585 		IPOS-TDSM
NORAD 69913 		3.235 14.32 1.9e-07
2026-10-13 16:12:27 UMBRA-12
NORAD 67371 		IPOS-TDSM
NORAD 69913 		1.975 11.36 8.0e-07
2026-10-14 16:23:13 SERT3
NORAD 68499 		IPOS-TDSM
NORAD 69913 		2.954 7.23 4.5e-07
2026-10-14 17:11:31 SERT3
NORAD 68499 		IPOS-TDSM
NORAD 69913 		4.053 7.21 2.4e-07
2026-10-15 07:00:13 IPOS-TDSM
NORAD 69913 		FENGYUN 1C DEB
NORAD 31768 		0.561 14.14 6.6e-06
2026-10-16 10:45:57 IPOS-TDSM
NORAD 69913 		OBJECT E
NORAD 100613 		2.218 14.95 3.2e-07
2026-10-16 18:49:05 IPOS-TDSM
NORAD 69913 		FRAMSAT-1
NORAD 100610 		4.461 14.95 7.9e-08
2026-10-16 21:58:36 AAC-AIS-SAT1
NORAD 55107 		IPOS-TDSM
NORAD 69913 		1.516 14.98 6.9e-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