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SNIPE D

In orbit NORAD 56744 EOVQ-9559-0511-0103-2591 South Korea

2023

Launch

102

Observations all time

Mission information
Spacecraft name
SNIPE D
Other names
KASI-SAT D, SNIPE-4
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2023-05-25 09:24:00
Separation time
2023-05-25 09:38:23
Last observers
Observer
Time of receipt
2026-09-10 17:22:25 UTC
2026-08-29 17:52:08 UTC
2026-06-24 16:42:56 UTC
2026-03-20 04:12:28 UTC
2026-03-10 18:04:46 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
420.83 km
Apogee
425.14 km
Inclination
97.5°
Period
93.1 min
Semi-major axis
6801.0 km
Velocity
7.65 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-15 14:36:39 UTC
Two-line elements (TLE)
1 56744U 23072B   26288.32600161  .00025583  00000-0  50990-3 0  9994
2 56744 97.5100 138.4689 0003211 239.8006 120.2926 15.46867063188650
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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
2026-10-16 07:32:29 SNIPE 4
NORAD 56744
CLEMENTINE
NORAD 25978
3.654 11.76 2.8e-07
2026-10-17 23:19:14 STARLINK-1168
NORAD 45072
SNIPE 4
NORAD 56744
2.020 14.45 1.5e-05
2026-10-18 18:43:36 SNIPE 4
NORAD 56744
STARLINK-32260
NORAD 61522
2.999 7.23 1.3e-05

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