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 56913U 26145.60930838 +.00000000 +00000-0 +24565-4 0 00008
2 56913 43.0024 356.1418 0001104 263.4474 96.6252 15.27577629 04
| Epoch (UTC): | 25 May 2026 14:37:24 |
| Eccentricity: | 0.0001104 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.1418° |
| argument of perigee: | 263.4474° |
| revolutions per day: | 15.27577629 |
| mean anomaly at epoch: | 96.6252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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