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 57058U 26145.10683284 +.00000000 +00000-0 +63845-4 0 00008
2 57058 43.0059 38.7418 0001579 268.7368 91.3303 15.27573985 02
| Epoch (UTC): | 25 May 2026 02:33:50 |
| Eccentricity: | 0.0001579 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 38.7418° |
| argument of perigee: | 268.7368° |
| revolutions per day: | 15.27573985 |
| mean anomaly at epoch: | 91.3303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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