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 57505U 26145.10258634 +.00000000 +00000-0 +15479-2 0 00000
2 57505 43.0018 294.7720 0008834 307.5184 52.4863 15.23837180 08
| Epoch (UTC): | 25 May 2026 02:27:43 |
| Eccentricity: | 0.0008834 |
| inclination: | 43.0018° |
| perigee height: | 488 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 294.7720° |
| argument of perigee: | 307.5184° |
| revolutions per day: | 15.23837180 |
| mean anomaly at epoch: | 52.4863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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