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 65769U 26145.12134310 +.00000000 +00000-0 +44661-3 0 00003
2 65769 51.9054 43.7712 0001040 104.8459 255.2616 14.75842796 09
| Epoch (UTC): | 25 May 2026 02:54:44 |
| Eccentricity: | 0.0001040 |
| inclination: | 51.9054° |
| perigee height: | 642 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 43.7712° |
| argument of perigee: | 104.8459° |
| revolutions per day: | 14.75842796 |
| mean anomaly at epoch: | 255.2616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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