View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 60189U 26145.37204146 +.00000000 +00000-0 +57793-5 0 00008
2 60189 53.1590 143.5541 0001120 82.1292 277.9853 15.69702645 06
| Epoch (UTC): | 25 May 2026 08:55:44 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.1590° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 143.5541° |
| argument of perigee: | 82.1292° |
| revolutions per day: | 15.69702645 |
| mean anomaly at epoch: | 277.9853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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