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

K-HERO

In orbit NORAD 66660 VFAW-1957-0148-9612-7991 South Korea

KSLV-2 Nuri

Carrier rocket

LC-2

Spaceport

157

Observations all time

Mission information
Spacecraft name
K-HERO
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
KSLV-2 Nuri
Spaceport
LC-2
Launch time
2025-11-26 15:54:00
Separation time
Last observers
Observer
Time of receipt
2026-03-02 10:16:33 UTC
2025-12-02 11:55:23 UTC
2025-12-02 11:53:53 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
571.78 km
Apogee
591.27 km
Inclination
97.8°
Period
96.4 min
Semi-major axis
6959.7 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:50 UTC
Two-line elements (TLE)
1 66660U 25274L   26283.04506592  .00001461  00000-0  14115-3 0  9993
2 66660 97.7516 210.9708 0013998 2.9210 357.2089 14.94311066 47383
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 12:50:52 K-HERO
NORAD 66660
FOREST-17 (TELPERION)
NORAD 68988
1.711 4.23 1.5e-06
2026-10-11 16:41:33 K-HERO
NORAD 66660
CZ-6A DEB
NORAD 55207
4.644 14.69 8.2e-08
2026-10-11 21:11:46 IRIDE-MS2-HEO-4
NORAD 64582
K-HERO
NORAD 66660
3.805 14.97 1.1e-07
2026-10-12 02:22:41 APRIZESAT 4
NORAD 35684
K-HERO
NORAD 66660
1.398 14.45 9.8e-07
2026-10-12 08:54:06 K-HERO
NORAD 66660
UNKNOWN
NORAD 89304
3.411 15.90 1.4e-07
2026-10-12 16:07:49 RCM-1
NORAD 44322
K-HERO
NORAD 66660
4.487 9.43 1.8e-07
2026-10-12 16:10:44 K-HERO
NORAD 66660
FENGYUN 1C DEB
NORAD 30912
2.434 4.93 7.1e-07
2026-10-13 00:06:54 KORSAT-7
NORAD 58463
K-HERO
NORAD 66660
3.195 13.82 2.2e-07
2026-10-13 04:04:15 K-HERO
NORAD 66660
OBJECT J
NORAD 44887
4.595 14.61 8.6e-08
2026-10-13 17:28:33 STARLINK-5611
NORAD 55761
K-HERO
NORAD 66660
4.753 15.07 2.1e-06
2026-10-13 19:04:43 STARLINK-5606
NORAD 55767
K-HERO
NORAD 66660
4.334 15.07 2.5e-06
2026-10-15 09:32:39 STARLINK-5595
NORAD 55765
K-HERO
NORAD 66660
4.616 15.04 2.2e-06
2026-10-16 09:23:21 SITRO-AIS 23
NORAD 61742
K-HERO
NORAD 66660
4.060 11.27 1.9e-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