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STPSAT-5

In orbit NORAD 43762 PEWC-8296-8648-1703-4023

Observations 0
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Falcon 9 Block 5 | Spaceflight SSO-A

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
STPSAT-5
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 | Spaceflight SSO-A
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
518.33 km
Apogee
520.57 km
Inclination
97.4°
Period
95.1 min
Semi-major axis
6897.6 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:42 UTC
Two-line elements (TLE)
1 43762U 18099E   26284.07925494  .00006338  00000-0  34760-3 0  9994
2 43762  97.3956 330.6904 0001625 313.5081  46.6016 15.14508671430405
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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
2026-10-13 13:50:46 STPSAT-5
NORAD 43762 		FENGYUN 1C DEB
NORAD 31536 		2.514 14.09 3.4e-07
2026-10-13 22:54:15 STPSAT-5
NORAD 43762 		COSMOS 886 DEB
NORAD 9824 		3.802 15.34 1.1e-07
2026-10-14 14:52:07 STPSAT-5
NORAD 43762 		GUANGCHUAN 02
NORAD 62112 		2.751 7.21 5.2e-07
2026-10-15 02:14:06 STPSAT-5
NORAD 43762 		COSMOS 1275 DEB
NORAD 42101 		4.513 14.90 8.2e-08
2026-10-15 03:01:40 STPSAT-5
NORAD 43762 		COSMOS 1275 DEB
NORAD 42101 		2.959 14.93 1.9e-07
2026-10-15 03:49:16 STPSAT-5
NORAD 43762 		COSMOS 1275 DEB
NORAD 42101 		3.639 14.90 1.3e-07
2026-10-15 04:36:50 STPSAT-5
NORAD 43762 		COSMOS 1275 DEB
NORAD 42101 		2.573 14.93 2.5e-07
2026-10-15 07:56:26 STPSAT-5
NORAD 43762 		SPACEMOBILE-009
NORAD 69590 		1.918 12.00 8.0e-07
2026-10-15 08:44:03 STPSAT-5
NORAD 43762 		SPACEMOBILE-009
NORAD 69590 		3.371 11.97 2.6e-07
2026-10-15 14:31:07 STPSAT-5
NORAD 43762 		TIROS 8 DEB
NORAD 19396 		2.458 14.86 2.8e-07
2026-10-15 23:37:54 STPSAT-5
NORAD 43762 		CZ-6A DEB
NORAD 64650 		4.944 10.65 1.4e-07
2026-10-16 07:29:20 STPSAT-5
NORAD 43762 		YUNYAO-1 45
NORAD 63346 		3.544 13.91 1.8e-07
2026-10-16 12:05:44 STPSAT-5
NORAD 43762 		STARLINK-3136
NORAD 49443 		3.299 7.49 1.1e-05
2026-10-16 19:05:07 STPSAT-5
NORAD 43762 		COSMOS 2251 DEB
NORAD 38220 		2.202 15.15 3.1e-07
2026-10-16 20:16:46 STPSAT-5
NORAD 43762 		FENGYUN 1C DEB
NORAD 35223 		3.716 2.21 3.2e-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