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 53800U 26145.49828855 +.00000000 +00000-0 +50999-3 0 00001
2 53800 53.2078 229.6613 0003379 33.6236 326.4991 15.58047487 00
| Epoch (UTC): | 25 May 2026 11:57:32 |
| Eccentricity: | 0.0003379 |
| inclination: | 53.2078° |
| perigee height: | 391 km |
| apogee height: | 396 km |
| right ascension of ascending node: | 229.6613° |
| argument of perigee: | 33.6236° |
| revolutions per day: | 15.58047487 |
| mean anomaly at epoch: | 326.4991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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