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SNUGLITE-III DURI

In orbit NORAD 66661 JAUW-7193-3193-5642-8786 South Korea

Time in UTC

23:28

Next pass · Чукотка · 71°

10.10 23:39

Scheduled · Великий Устюг

1035

Observations over 30 days

50%

Successful observations

16k

Frames, latest 2026-10-10 22:15 UTC

Mission information
Spacecraft name
SNUGLITE-III DURI
Other names
DS0DH
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
2026-10-10 22:15:01 UTC
2026-10-10 22:12:18 UTC
2026-10-10 20:38:41 UTC
2026-10-10 19:01:31 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
571.32 km
Apogee
591.73 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 20:56:59 UTC
Two-line elements (TLE)
1 66661U 25274M   26283.56710658  .00001678  00000-0  16124-3 0  9993
2 66661 97.7514 211.5057 0014603 2.0781 358.0497 14.94313873 47463
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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
2026-10-10 22:44:24 CONNECTA IOT-8
NORAD 62695
SNUGLITE-III
NORAD 66661
4.230 14.37 1.1e-07
2026-10-11 00:20:51 CONNECTA IOT-8
NORAD 62695
SNUGLITE-III
NORAD 66661
4.714 14.37 8.8e-08
2026-10-11 07:26:16 STARLINK-5499
NORAD 55764
SNUGLITE-III
NORAD 66661
3.403 15.03 4.1e-06
2026-10-12 17:15:54 SNUGLITE-III
NORAD 66661
CZ-6A DEB
NORAD 55208
4.998 14.76 7.0e-08
2026-10-13 05:47:35 LEMUR-2-SEJONG-2
NORAD 64586
SNUGLITE-III
NORAD 66661
2.425 14.98 2.7e-07
2026-10-14 07:58:33 KX-09
NORAD 44520
SNUGLITE-III
NORAD 66661
3.137 10.11 3.5e-07
2026-10-14 10:34:06 PE2_FLT2 (TYVAK-0262)
NORAD 59104
SNUGLITE-III
NORAD 66661
2.875 14.67 2.2e-07
2026-10-14 20:23:30 STARLINK-5833
NORAD 55773
SNUGLITE-III
NORAD 66661
4.975 15.05 1.9e-06
2026-10-15 06:21:56 TIANQIN 1 (CAS-6)
NORAD 44879
SNUGLITE-III
NORAD 66661
4.951 14.65 7.4e-08
2026-10-15 13:43:13 SNUGLITE-III
NORAD 66661
FENGYUN 1C DEB
NORAD 30297
3.147 4.06 4.3e-07
2026-10-15 15:41:41 SNUGLITE-III
NORAD 66661
COSMOS 2251 DEB
NORAD 35898
3.216 15.11 1.5e-07
2026-10-15 17:05:59 SNUGLITE-III
NORAD 66661
METHANESAT
NORAD 59101
4.049 14.66 1.1e-07
2026-10-15 20:10:38 SNUGLITE-III
NORAD 66661
UNKNOWN
NORAD 89029
2.152 2.00 9.5e-07
2026-10-15 20:12:34 SNUGLITE-III
NORAD 66661
PIESAT-2 OBJECT B
NORAD 100750
2.826 11.68 3.8e-07
2026-10-16 04:30:18 LEMUR-2-KRISH
NORAD 64561
SNUGLITE-III
NORAD 66661
4.856 14.98 6.7e-08
2026-10-16 15:43:53 SNUGLITE-III
NORAD 66661
CZ-2C R/B
NORAD 58499
0.597 14.96 4.5e-06
2026-10-16 19:30:51 SNUGLITE-III
NORAD 66661
FENGYUN 1C DEB
NORAD 32114
3.580 10.79 2.5e-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