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 57605U 26145.31438463 +.00000000 +00000-0 +10928-3 0 00009
2 57605 43.0020 8.9762 0001418 266.6401 93.4289 15.27586875 04
| Epoch (UTC): | 25 May 2026 07:32:42 |
| Eccentricity: | 0.0001418 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.9762° |
| argument of perigee: | 266.6401° |
| revolutions per day: | 15.27586875 |
| mean anomaly at epoch: | 93.4289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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