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 53765U 26145.58424844 +.00000000 +00000-0 +00000-0 0 00006
2 53765 0.0610 104.6440 0002842 298.9017 52.6559 1.00269263 07
| Epoch (UTC): | 25 May 2026 14:01:19 |
| Eccentricity: | 0.0002842 |
| inclination: | 0.0610° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 104.6440° |
| argument of perigee: | 298.9017° |
| revolutions per day: | 1.00269263 |
| mean anomaly at epoch: | 52.6559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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