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 56699U 26145.49022152 +.00000000 +00000-0 +59734-4 0 00003
2 56699 43.0037 207.7287 0001389 256.0073 104.0624 15.26743252 05
| Epoch (UTC): | 25 May 2026 11:45:55 |
| Eccentricity: | 0.0001389 |
| inclination: | 43.0037° |
| perigee height: | 485 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 207.7287° |
| argument of perigee: | 256.0073° |
| revolutions per day: | 15.26743252 |
| mean anomaly at epoch: | 104.0624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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