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 57220U 26145.50068185 +.00000000 +00000-0 +43763-4 0 00007
2 57220 43.0029 320.2612 0001608 268.1185 91.9482 15.26744358 06
| Epoch (UTC): | 25 May 2026 12:00:58 |
| Eccentricity: | 0.0001608 |
| inclination: | 43.0029° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 320.2612° |
| argument of perigee: | 268.1185° |
| revolutions per day: | 15.26744358 |
| mean anomaly at epoch: | 91.9482° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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