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 56916U 26145.02725567 +.00000000 +00000-0 +10501-4 0 00003
2 56916 43.0012 359.5075 0001000 251.2614 108.8129 15.27576654 02
| Epoch (UTC): | 25 May 2026 00:39:14 |
| Eccentricity: | 0.0001000 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 359.5075° |
| argument of perigee: | 251.2614° |
| revolutions per day: | 15.27576654 |
| mean anomaly at epoch: | 108.8129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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