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 56466U 26145.42567969 +.00000000 +00000-0 +69112-4 0 00009
2 56466 69.9993 310.8423 0003041 272.3346 87.7465 14.98340694 05
| Epoch (UTC): | 25 May 2026 10:12:58 |
| Eccentricity: | 0.0003041 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.8423° |
| argument of perigee: | 272.3346° |
| revolutions per day: | 14.98340694 |
| mean anomaly at epoch: | 87.7465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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