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SJSAT-4

In orbit NORAD 66651 EQML-6882-0922-9942-3929 South Korea

KSLV-2 Nuri

Carrier rocket

LC-2

Spaceport

0

Observations all time

Mission information
Spacecraft name
SJSAT-4
Other names
SEJONG-4
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
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
576.50 km
Apogee
592.34 km
Inclination
97.8°
Period
96.4 min
Semi-major axis
6962.6 km
Velocity
7.55 km/s
Orbital elements
TLE source
Space-Track.org
TLE updated
2026-10-08 08:46:45 UTC
Two-line elements (TLE)
1 66650U 25274A   26280.73580210  .00001889  00000-0  18522-3 0  9994
2 66650 97.7503 208.1281 0011375 348.5846 11.5114 14.93380725 47009
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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 04:19:06 OBJECT B
NORAD 66651
PEARL-1B
NORAD 68980
1.737 4.20 1.4e-06
2026-10-11 09:49:48 BRO-14
NORAD 60551
OBJECT B
NORAD 66651
3.876 14.32 1.3e-07
2026-10-11 14:38:22 AAC-AIS-SAT1
NORAD 55107
OBJECT B
NORAD 66651
1.738 14.46 6.3e-07
2026-10-11 21:12:04 OBJECT B
NORAD 66651
INHA-ROSAT
NORAD 66653
2.918 0.02 5.2e-07
2026-10-12 12:28:15 OBJECT B
NORAD 66651
CESARIO
NORAD 100642
1.888 3.88 1.2e-06
2026-10-12 17:35:58 IRIDE-MS2-HEO-9
NORAD 64585
OBJECT B
NORAD 66651
3.442 14.97 1.3e-07
2026-10-12 22:07:05 OBJECT B
NORAD 66651
ICEYE-X77
NORAD 69892
4.080 3.70 2.6e-07
2026-10-13 01:20:01 OBJECT B
NORAD 66651
REPLICATOR 2
NORAD 69927
0.812 3.70 6.5e-06
2026-10-13 14:11:44 OBJECT B
NORAD 66651
HYPERION GR-1
NORAD 69883
2.799 3.71 5.5e-07
2026-10-13 16:52:06 OBJECT B
NORAD 66651
CZ-2D R/B
NORAD 68141
1.437 9.61 1.7e-06
2026-10-14 13:09:21 OBJECT B
NORAD 66651
COSMOS 2251 DEB
NORAD 35898
3.128 15.06 1.5e-07
2026-10-14 19:49:47 ION SCV-012
NORAD 60573
OBJECT B
NORAD 66651
0.761 14.24 3.5e-06
2026-10-15 14:23:24 RCM-2
NORAD 44324
OBJECT B
NORAD 66651
2.774 9.47 4.6e-07
2026-10-15 14:25:37 OBJECT B
NORAD 66651
SPEAR-1A
NORAD 69900
3.021 3.71 4.7e-07
2026-10-16 15:29:06 PE2_FLT2 (TYVAK-0262)
NORAD 59104
OBJECT B
NORAD 66651
3.463 14.66 1.5e-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