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 65700U 26145.58486579 +.00000000 +00000-0 +65836-3 0 00002
2 65700 53.1614 347.2908 0001307 99.4497 260.6653 15.34411498 04
| Epoch (UTC): | 25 May 2026 14:02:12 |
| Eccentricity: | 0.0001307 |
| inclination: | 53.1614° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 347.2908° |
| argument of perigee: | 99.4497° |
| revolutions per day: | 15.34411498 |
| mean anomaly at epoch: | 260.6653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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