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 53825U 26145.49016778 +.00000000 +00000-0 +51325-4 0 00006
2 53825 53.2152 319.4902 0001274 96.2512 263.8625 15.08842132 06
| Epoch (UTC): | 25 May 2026 11:45:50 |
| Eccentricity: | 0.0001274 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 319.4902° |
| argument of perigee: | 96.2512° |
| revolutions per day: | 15.08842132 |
| mean anomaly at epoch: | 263.8625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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