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 57702U 26145.43413477 +.00000000 +00000-0 +41007-4 0 00001
2 57702 43.0049 44.1525 0000972 267.9198 92.1542 15.27577765 09
| Epoch (UTC): | 25 May 2026 10:25:09 |
| Eccentricity: | 0.0000972 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 44.1525° |
| argument of perigee: | 267.9198° |
| revolutions per day: | 15.27577765 |
| mean anomaly at epoch: | 92.1542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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