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 57152U 26145.18655397 +.00000000 +00000-0 +20330-4 0 00007
2 57152 43.0029 191.2299 0001766 275.7909 84.2741 15.27578478 02
| Epoch (UTC): | 25 May 2026 04:28:38 |
| Eccentricity: | 0.0001766 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 191.2299° |
| argument of perigee: | 275.7909° |
| revolutions per day: | 15.27578478 |
| mean anomaly at epoch: | 84.2741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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