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 57497U 26145.44818681 +.00000000 +00000-0 +59487-4 0 00000
2 57497 43.0027 302.6572 0001480 251.7517 108.3174 15.27568581 08
| Epoch (UTC): | 25 May 2026 10:45:23 |
| Eccentricity: | 0.0001480 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.6572° |
| argument of perigee: | 251.7517° |
| revolutions per day: | 15.27568581 |
| mean anomaly at epoch: | 108.3174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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