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 65096U 26144.90556823 +.00000000 +00000-0 +49127-3 0 00000
2 65096 53.1593 30.1665 0001075 79.3256 280.7870 15.42179791 08
| Epoch (UTC): | 24 May 2026 21:44:01 |
| Eccentricity: | 0.0001075 |
| inclination: | 53.1593° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 30.1665° |
| argument of perigee: | 79.3256° |
| revolutions per day: | 15.42179791 |
| mean anomaly at epoch: | 280.7870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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