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 56788U 26145.33597339 +.00000000 +00000-0 -36437-3 0 00004
2 56788 69.9983 131.2346 0003405 268.0567 92.0202 14.98340000 00
| Epoch (UTC): | 25 May 2026 08:03:48 |
| Eccentricity: | 0.0003405 |
| inclination: | 69.9983° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 131.2346° |
| argument of perigee: | 268.0567° |
| revolutions per day: | 14.98340000 |
| mean anomaly at epoch: | 92.0202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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