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 26104.21102601 +.00000000 +00000-0 +24268-3 0 00008
2 39057 82.4945 260.1587 0028095 162.7864 197.4175 12.42994631 00
| Epoch (UTC): | 14 April 2026 05:03:52 |
| Eccentricity: | 0.0028095 |
| inclination: | 82.4945° |
| perigee height: | 1472 km |
| apogee height: | 1516 km |
| right ascension of ascending node: | 260.1587° |
| argument of perigee: | 162.7864° |
| revolutions per day: | 12.42994631 |
| mean anomaly at epoch: | 197.4175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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