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Kita-36

In orbit NORAD 69909 QEQN-2303-2903-1759-3791

Observations 15
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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

15

Observations all time

Mission information
Spacecraft name
Kita-36
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
2026-07-07 08:14:56
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
586.32 km
Apogee
593.83 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6968.2 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:21 UTC
Two-line elements (TLE)
1 69909U 26156AS  26282.53577679  .00001688  00000-0  17386-3 0  9993
2 69909  97.7432 181.3554 0005390 168.2848 191.8497 14.91564642 14048
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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 03:59:05 KITA-36
NORAD 69909 		DELTA 1 DEB
NORAD 13826 		2.454 13.32 4.1e-07
2026-10-12 08:53:59 KITA-36
NORAD 69909 		CZ-6A DEB
NORAD 61809 		3.791 8.74 2.6e-07
2026-10-12 20:53:34 KITA-36
NORAD 69909 		COSMOS 2251 DEB
NORAD 36441 		3.324 12.43 2.5e-07
2026-10-13 17:28:13 KITA-36
NORAD 69909 		CZ-6A DEB
NORAD 54579 		3.987 14.97 1.0e-07
2026-10-13 20:15:50 LEMUR-2-SONNENBLUME
NORAD 67367 		KITA-36
NORAD 69909 		3.524 11.32 2.5e-07
2026-10-13 20:19:42 KITA-36
NORAD 69909 		FENGYUN 1C DEB
NORAD 31492 		1.652 7.21 1.4e-06
2026-10-14 09:58:09 LEMUR-2-EMARCHIA
NORAD 68492 		KITA-36
NORAD 69909 		4.360 7.22 2.1e-07
2026-10-14 13:46:54 KITA-36
NORAD 69909 		SS 1
NORAD 10529 		4.894 14.94 7.2e-08
2026-10-15 01:10:56 KITA-36
NORAD 69909 		NOAA 17 DEB
NORAD 48765 		1.695 14.16 7.2e-07
2026-10-16 00:30:40 KITA-36
NORAD 69909 		COSMOS 397 DEB
NORAD 5144 		1.988 14.00 5.6e-07
2026-10-16 14:25:03 ION SCV-018
NORAD 64575 		KITA-36
NORAD 69909 		1.808 14.28 6.2e-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