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 57186U 26145.46160324 +.00000000 +00000-0 +30381-3 0 00002
2 57186 97.5161 211.5047 0018947 169.0255 191.1402 15.28458378 04
| Epoch (UTC): | 25 May 2026 11:04:42 |
| Eccentricity: | 0.0018947 |
| inclination: | 97.5161° |
| perigee height: | 467 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 211.5047° |
| argument of perigee: | 169.0255° |
| revolutions per day: | 15.28458378 |
| mean anomaly at epoch: | 191.1402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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