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

SPIRONE

In orbit NORAD 66657 WNIW-3579-8441-1864-2418 South Korea

Time in UTC

—

No observations scheduled

1

Observations over 30 days

61%

Successful observations

13k

Frames, latest 2026-10-10 23:11 UTC

Mission information
Spacecraft name
SPIRONE
Other names
Sejong university's Promising Eyes on envIRONment
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
KSLV-2 Nuri
Spaceport
LC-2
Launch time
2025-11-26 15:54:00
Separation time
Last observers
Observer
Time of receipt
2026-09-30 08:53:21 UTC
2026-09-04 09:08:40 UTC
2026-08-13 22:59:30 UTC
2026-07-15 22:49:07 UTC
2026-06-26 09:04:23 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
574.38 km
Apogee
591.14 km
Inclination
97.8°
Period
96.4 min
Semi-major axis
6960.9 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:59 UTC
Two-line elements (TLE)
1 66657U 25274H   26283.54020822  .00002055  00000-0  19828-3 0  9997
2 66657 97.7508 211.2153 0011938 358.2365 1.8811 14.93919837 47449
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 15:56:00 PUJIANG 2 (PJ-2)
NORAD 52151
SPIRONE
NORAD 66657
3.805 11.63 2.1e-07
2026-10-11 23:09:57 PUJIANG 2 (PJ-2)
NORAD 52151
SPIRONE
NORAD 66657
4.788 11.65 1.3e-07
2026-10-12 07:37:21 SPIRONE
NORAD 66657
BRITE-PL1 (LEM)
NORAD 39431
1.982 15.03 4.0e-07
2026-10-13 03:55:18 SPIRONE
NORAD 66657
PEGASUS DEB
NORAD 24239
3.079 15.16 1.6e-07
2026-10-13 15:14:37 SPIRONE
NORAD 66657
DELTA 1 DEB
NORAD 37667
4.496 13.30 1.2e-07
2026-10-14 03:59:15 SPIRONE
NORAD 66657
UNKNOWN
NORAD 270138
4.236 14.83 9.5e-08
2026-10-14 05:08:03 SPIRONE
NORAD 66657
COSMOS 2251 DEB
NORAD 38001
2.567 5.31 6.3e-07
2026-10-14 05:35:40 SPIRONE
NORAD 66657
UNKNOWN
NORAD 270138
2.590 14.83 2.5e-07
2026-10-14 06:23:56 SPIRONE
NORAD 66657
UNKNOWN
NORAD 270138
4.528 14.79 8.3e-08
2026-10-14 08:00:22 SPIRONE
NORAD 66657
UNKNOWN
NORAD 270138
3.496 14.79 1.4e-07
2026-10-14 13:49:29 SPIRONE
NORAD 66657
GRUS-3C
NORAD 69891
3.393 3.74 3.7e-07
2026-10-14 17:20:54 IRIDE-MS2-HEO-8
NORAD 64587
SPIRONE
NORAD 66657
4.117 14.97 9.4e-08
2026-10-16 11:51:55 SPIRONE
NORAD 66657
CZ-6A DEB
NORAD 61102
4.364 1.49 2.3e-07
2026-10-16 14:49:03 COSMOS 2523
NORAD 42986
SPIRONE
NORAD 66657
2.438 9.66 5.9e-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