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 57812U 26145.35813147 +.00000000 +00000-0 -34676-4 0 00007
2 57812 43.0042 161.2073 0001341 261.8857 98.1842 15.27582335 07
| Epoch (UTC): | 25 May 2026 08:35:42 |
| Eccentricity: | 0.0001341 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 161.2073° |
| argument of perigee: | 261.8857° |
| revolutions per day: | 15.27582335 |
| mean anomaly at epoch: | 98.1842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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