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 53419U 26145.38987667 +.00000000 +00000-0 +56392-3 0 00005
2 53419 53.2129 129.7971 0001263 86.3205 273.7931 15.08797995 00
| Epoch (UTC): | 25 May 2026 09:21:25 |
| Eccentricity: | 0.0001263 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 129.7971° |
| argument of perigee: | 86.3205° |
| revolutions per day: | 15.08797995 |
| mean anomaly at epoch: | 273.7931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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