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 57116U 26145.23682468 +.00000000 +00000-0 -19764-4 0 00002
2 57116 43.0039 208.8943 0001938 285.4142 74.6495 15.26739627 05
| Epoch (UTC): | 25 May 2026 05:41:01 |
| Eccentricity: | 0.0001938 |
| inclination: | 43.0039° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 208.8943° |
| argument of perigee: | 285.4142° |
| revolutions per day: | 15.26739627 |
| mean anomaly at epoch: | 74.6495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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