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Starlink satellite close conjunction forecast

Results from latest analysis of positions : searching for near misses (< 1 km) over the next 24 hours. Includes nearest approaches to ISS and CSS regardless of distance

near conjunctions forecast
UTC Distance (km) Obj1 Obj2 ΔAlt kmh
2024-04-14T07:36:27.119Z (intl. Space Station)
19.741255445927219.273752
2024-04-14T06:05:02.709Z (China Space Station)
0.00048274582160.000
2024-04-14T06:13:12.999Z
0.37952549547720.3820106
2024-04-14T15:47:14.169Z
0.23753798542060.138672
2024-04-14T17:25:19.969Z
0.64454082547990.414701
2024-04-14T14:17:28.919Z
0.27749451497370.2616059
2024-04-14T09:36:21.819Z
0.49752124528310.456034
2024-04-14T12:05:20.289Z
0.54751861535740.325184
2024-04-14T11:52:38.839Z
0.51046704587080.331052
2024-04-14T12:55:22.209Z
0.38151861521220.3813699
2024-04-14T08:14:51.049Z
0.28749428537870.288243
2024-04-14T16:12:26.659Z
0.12151805526100.0811267
2024-04-14T09:54:51.319Z
0.41351996540950.386213
2024-04-14T06:54:03.499Z
0.37951732541700.206585
2024-04-14T13:17:51.799Z
0.62651732548040.109842
2024-04-14T10:12:45.529Z
0.31849771532810.267474
2024-04-14T08:45:38.699Z
0.29752663536330.0614802
2024-04-14T10:40:52.749Z
0.51852610542050.1510395
2024-04-14T13:57:57.459Z
0.83352683547860.5614485
2024-04-14T17:09:45.379Z
0.54244725477910.265096
2024-04-14T07:38:11.299Z
0.44253842539680.4412852
2024-04-14T12:52:01.509Z
0.48553390535780.0710879
2024-04-14T17:04:08.349Z
0.74351124537270.234336
2024-04-14T09:41:16.479Z
0.46853787554730.311108
2024-04-14T11:50:50.999Z
0.15749174572280.169441
2024-04-14T17:15:46.379Z
0.54459027591550.5111231
2024-04-14T17:40:06.469Z
0.53058674591640.521252
2024-04-14T14:38:30.809Z
0.77746149536300.538751
2024-04-14T16:55:33.409Z
0.55645734581630.4522807

Forecast run at: Sun, 14 Apr 2024 10:02:58 UTC

About: twice a day the latest TLEs (fixes) are propagated forward if necessary by 1/100th of a second steps to identify the closest any pair of satellites will be to each other. Since TLEs contain a small amount of position uncertainty and the orbit propagation model is also slightly imperfect the identified near pass may be inaccurate. In addition, satellites undergoing thrust currently will not be placed correctly hours into the future.