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GYEONGGISAT-1

In orbit NORAD 66771 EJND-0405-5952-6633-3287

Falcon 9

Carrier rocket

База Вандерберг

Spaceport

0

Observations all time

Mission information
Spacecraft name
GYEONGGISAT-1
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
Spaceport
База Вандерберг
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
496.13 km
Apogee
498.80 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6875.6 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:20 UTC
Two-line elements (TLE)
1 66771U 25276DK  26282.53040663  .00004987  00000-0  22294-3 0  9996
2 66771 97.4138 354.7753 0001942 148.0659 212.0695 15.21771550 47824
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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 14:01:35 GAOFEN-11 04
NORAD 54818
GYEONGGISAT-1
NORAD 66771
2.425 7.53 6.6e-07
2026-10-11 14:27:29 TOMORROW-S6
NORAD 63225
GYEONGGISAT-1
NORAD 66771
3.976 15.10 9.9e-08
2026-10-11 14:47:43 GYEONGGISAT-1
NORAD 66771
SL-3 R/B
NORAD 13068
4.131 10.81 5.3e-07
2026-10-11 23:03:41 GYEONGGISAT-1
NORAD 66771
BSLT-3
NORAD 69009
3.856 15.09 1.1e-07
2026-10-12 00:38:22 GYEONGGISAT-1
NORAD 66771
BSLT-3
NORAD 69009
2.219 15.09 3.2e-07
2026-10-12 02:13:02 GYEONGGISAT-1
NORAD 66771
BSLT-3
NORAD 69009
1.473 15.09 7.2e-07
2026-10-12 03:47:42 GYEONGGISAT-1
NORAD 66771
BSLT-3
NORAD 69009
2.577 15.09 2.4e-07
2026-10-12 04:14:33 FLOCK 4H-2
NORAD 66705
GYEONGGISAT-1
NORAD 66771
0.402 0.03 2.7e-05
2026-10-12 04:35:02 GYEONGGISAT-1
NORAD 66771
BSLT-3
NORAD 69009
4.275 15.10 8.6e-08
2026-10-12 05:01:51 FLOCK 4H-2
NORAD 66705
GYEONGGISAT-1
NORAD 66771
1.677 0.03 1.6e-06
2026-10-12 05:22:22 GYEONGGISAT-1
NORAD 66771
BSLT-3
NORAD 69009
4.284 15.09 8.6e-08
2026-10-12 06:09:42 GYEONGGISAT-1
NORAD 66771
BSLT-3
NORAD 69009
2.589 15.10 2.3e-07
2026-10-12 07:44:22 GYEONGGISAT-1
NORAD 66771
BSLT-3
NORAD 69009
1.549 15.10 6.6e-07
2026-10-12 09:19:02 GYEONGGISAT-1
NORAD 66771
BSLT-3
NORAD 69009
2.320 15.10 2.9e-07
2026-10-12 10:53:42 GYEONGGISAT-1
NORAD 66771
BSLT-3
NORAD 69009
3.961 15.10 1.0e-07
2026-10-13 10:14:22 GYEONGGISAT-1
NORAD 66771
DCS-1
NORAD 67263
3.664 0.12 3.3e-07
2026-10-14 10:41:29 LEMUR-2-DEANANDMAEVE
NORAD 66680
GYEONGGISAT-1
NORAD 66771
4.031 0.12 2.7e-07
2026-10-15 20:37:34 CSTP 1.1 (STC 1.1)
NORAD 57202
GYEONGGISAT-1
NORAD 66771
2.913 1.85 5.2e-07
2026-10-15 20:47:55 GYEONGGISAT-1
NORAD 66771
LVM3 R/B
NORAD 67233
2.953 13.52 2.8e-07
2026-10-16 10:14:03 GYEONGGISAT-1
NORAD 66771
IRIDIUM 33 DEB
NORAD 46971
3.396 15.19 1.3e-07
2026-10-16 11:01:22 GYEONGGISAT-1
NORAD 66771
IRIDIUM 33 DEB
NORAD 46971
0.353 15.22 1.2e-05
2026-10-16 16:16:54 GYEONGGISAT-1
NORAD 66771
SL-8 DEB
NORAD 11114
4.991 12.10 1.2e-07
2026-10-16 17:04:17 GYEONGGISAT-1
NORAD 66771
SL-8 DEB
NORAD 11114
3.164 12.14 2.9e-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