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 39057U 26145.58297161 +.00000000 +00000-0 +22700-3 0 00008
2 39057 82.4988 234.4177 0028644 75.7581 284.6677 12.42995678 03
| Epoch (UTC): | 25 May 2026 13:59:28 |
| Eccentricity: | 0.0028644 |
| inclination: | 82.4988° |
| perigee height: | 1471 km |
| apogee height: | 1516 km |
| right ascension of ascending node: | 234.4177° |
| argument of perigee: | 75.7581° |
| revolutions per day: | 12.42995678 |
| mean anomaly at epoch: | 284.6677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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