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 57739U 26145.20029266 +.00000000 +00000-0 +28263-3 0 00003
2 57739 43.0018 71.5594 0001396 260.9134 99.1559 15.27586882 04
| Epoch (UTC): | 25 May 2026 04:48:25 |
| Eccentricity: | 0.0001396 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 71.5594° |
| argument of perigee: | 260.9134° |
| revolutions per day: | 15.27586882 |
| mean anomaly at epoch: | 99.1559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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