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 65308U 26145.60868020 +.00000000 +00000-0 +64437-4 0 00001
2 65308 50.0016 286.9851 0000531 95.5497 264.5436 13.29322869 08
| Epoch (UTC): | 25 May 2026 14:36:29 |
| Eccentricity: | 0.0000531 |
| inclination: | 50.0016° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 286.9851° |
| argument of perigee: | 95.5497° |
| revolutions per day: | 13.29322869 |
| mean anomaly at epoch: | 264.5436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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