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 53857U 26145.43581698 +.00000000 +00000-0 -60901-4 0 00004
2 53857 53.2131 309.1715 0001236 93.1039 267.0094 15.08844229 09
| Epoch (UTC): | 25 May 2026 10:27:34 |
| Eccentricity: | 0.0001236 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 309.1715° |
| argument of perigee: | 93.1039° |
| revolutions per day: | 15.08844229 |
| mean anomaly at epoch: | 267.0094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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