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 65312U 26145.66702704 +.00000000 +00000-0 +75285-4 0 00001
2 65312 50.0036 286.6723 0000681 81.6558 278.4391 13.29322020 03
| Epoch (UTC): | 25 May 2026 16:00:31 |
| Eccentricity: | 0.0000681 |
| inclination: | 50.0036° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 286.6723° |
| argument of perigee: | 81.6558° |
| revolutions per day: | 13.29322020 |
| mean anomaly at epoch: | 278.4391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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