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 53738U 26145.37603966 +.00000000 +00000-0 +43018-4 0 00007
2 53738 53.2150 279.6367 0001268 84.5940 275.5197 15.08840851 07
| Epoch (UTC): | 25 May 2026 09:01:29 |
| Eccentricity: | 0.0001268 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 279.6367° |
| argument of perigee: | 84.5940° |
| revolutions per day: | 15.08840851 |
| mean anomaly at epoch: | 275.5197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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