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 57044U 26145.62230451 +.00000000 +00000-0 +46244-3 0 00007
2 57044 97.4894 258.6926 0008069 154.5049 205.6594 15.35878172 00
| Epoch (UTC): | 25 May 2026 14:56:07 |
| Eccentricity: | 0.0008069 |
| inclination: | 97.4894° |
| perigee height: | 453 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 258.6926° |
| argument of perigee: | 154.5049° |
| revolutions per day: | 15.35878172 |
| mean anomaly at epoch: | 205.6594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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