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 56828U 26144.70863156 +.00000000 +00000-0 +17650-4 0 00008
2 56828 43.0045 37.7994 0001524 277.0195 83.0484 15.27582257 00
| Epoch (UTC): | 24 May 2026 17:00:25 |
| Eccentricity: | 0.0001524 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.7994° |
| argument of perigee: | 277.0195° |
| revolutions per day: | 15.27582257 |
| mean anomaly at epoch: | 83.0484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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