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 53925U 26145.48182270 +.00000000 +00000-0 +46894-4 0 00002
2 53925 53.2137 328.9887 0001326 92.8307 267.2837 15.08835846 06
| Epoch (UTC): | 25 May 2026 11:33:49 |
| Eccentricity: | 0.0001326 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 328.9887° |
| argument of perigee: | 92.8307° |
| revolutions per day: | 15.08835846 |
| mean anomaly at epoch: | 267.2837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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