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 57294U 26145.36332137 +.00000000 +00000-0 +71468-5 0 00007
2 57294 43.0012 150.1653 0001765 279.9743 80.0909 15.27584105 04
| Epoch (UTC): | 25 May 2026 08:43:10 |
| Eccentricity: | 0.0001765 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.1653° |
| argument of perigee: | 279.9743° |
| revolutions per day: | 15.27584105 |
| mean anomaly at epoch: | 80.0909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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