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

KOYO

In orbit NORAD 69916 YZNT-7399-1272-5956-2962 Taiwan

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

49

Observations all time

Mission information
Spacecraft name
KOYO
Frequency usage status
Violator
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
2026-07-07 07:12:00
Separation time
2026-07-07 08:06:59
Last observers
Observer
Time of receipt
2026-08-11 09:23:04 UTC
2026-08-10 20:39:49 UTC
2026-08-03 08:03:30 UTC
2026-08-03 06:27:41 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
589.12 km
Apogee
593.35 km
Inclination
97.7°
Period
96.6 min
Semi-major axis
6969.4 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:57:00 UTC
Two-line elements (TLE)
1 69916U 26156AZ  26283.50380862  .00002029  00000-0  20984-3 0  9993
2 69916 97.7418 182.2168 0003082 148.1645 211.9761 14.91194695 14189
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
2026-10-11 07:07:07 KOYO
NORAD 69916
ELECTRON KICK STAGE R/B
NORAD 61226
4.651 14.24 9.3e-08
2026-10-12 14:31:29 PADRE
NORAD 64559
KOYO
NORAD 69916
3.956 14.35 1.3e-07
2026-10-12 22:56:34 KOYO
NORAD 69916
DELTA 2 R/B(1)
NORAD 21891
4.702 12.41 6.1e-07
2026-10-13 04:47:55 KOYO
NORAD 69916
SCOUT X-4 R/B
NORAD 1815
3.889 6.56 3.6e-07
2026-10-14 09:37:21 CAPELLA-11 (ACADIA-1)
NORAD 57693
KOYO
NORAD 69916
4.552 14.46 9.2e-08
2026-10-14 13:13:08 KOYO
NORAD 69916
CZ-2C R/B
NORAD 58499
4.867 14.19 8.7e-08
2026-10-15 00:50:40 FIREFLY-3
NORAD 62710
KOYO
NORAD 69916
2.712 14.98 2.1e-07
2026-10-15 11:39:18 KOYO
NORAD 69916
SL-8 R/B
NORAD 20775
4.468 13.96 5.4e-07
2026-10-15 14:56:35 KOYO
NORAD 69916
COROT
NORAD 29678
2.969 14.60 2.1e-07
2026-10-16 00:34:37 KOYO
NORAD 69916
SICH-1
NORAD 23657
3.208 11.59 3.9e-06
2026-10-16 07:25:36 KOYO
NORAD 69916
03B MPOWER F12
NORAD 100687
2.817 13.43 3.5e-07
2026-10-16 08:53:31 KOYO
NORAD 69916
CBERS 1 DEB
NORAD 35387
1.375 14.95 8.5e-07
2026-10-16 10:30:06 KOYO
NORAD 69916
CBERS 1 DEB
NORAD 35387
3.387 14.95 1.4e-07
2026-10-16 22:19:46 KOYO
NORAD 69916
FENGYUN 1C DEB
NORAD 32221
1.609 10.88 1.3e-06

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