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 57069U 26145.37547081 +.00000000 +00000-0 -33728-4 0 00001
2 57069 43.0057 23.4568 0001070 268.9439 91.1290 15.27565377 05
| Epoch (UTC): | 25 May 2026 09:00:40 |
| Eccentricity: | 0.0001070 |
| inclination: | 43.0057° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 23.4568° |
| argument of perigee: | 268.9439° |
| revolutions per day: | 15.27565377 |
| mean anomaly at epoch: | 91.1290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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