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 56775U 26145.33575209 +.00000000 +00000-0 +16651-4 0 00008
2 56775 69.9993 111.3512 0003519 266.1362 93.9395 14.98331922 05
| Epoch (UTC): | 25 May 2026 08:03:28 |
| Eccentricity: | 0.0003519 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 111.3512° |
| argument of perigee: | 266.1362° |
| revolutions per day: | 14.98331922 |
| mean anomaly at epoch: | 93.9395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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