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 56950U 26145.36854075 +.00000000 +00000-0 +24426-3 0 00005
2 56950 97.6177 280.3935 0004045 90.1903 269.9794 15.18320627 00
| Epoch (UTC): | 25 May 2026 08:50:41 |
| Eccentricity: | 0.0004045 |
| inclination: | 97.6177° |
| perigee height: | 508 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 280.3935° |
| argument of perigee: | 90.1903° |
| revolutions per day: | 15.18320627 |
| mean anomaly at epoch: | 269.9794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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