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 65402U 26145.59305176 +.00000000 +00000-0 +51810-4 0 00003
2 65402 97.4505 16.9809 0002668 77.5881 282.5645 15.05660939 06
| Epoch (UTC): | 25 May 2026 14:13:59 |
| Eccentricity: | 0.0002668 |
| inclination: | 97.4505° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.9809° |
| argument of perigee: | 77.5881° |
| revolutions per day: | 15.05660939 |
| mean anomaly at epoch: | 282.5645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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