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 53025U 26145.16446814 +.00000000 +00000-0 +28089-4 0 00001
2 53025 53.2133 100.8105 0001304 72.5201 287.5933 15.08837332 01
| Epoch (UTC): | 25 May 2026 03:56:50 |
| Eccentricity: | 0.0001304 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.8105° |
| argument of perigee: | 72.5201° |
| revolutions per day: | 15.08837332 |
| mean anomaly at epoch: | 287.5933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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