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 65364U 26145.48464560 +.00000000 +00000-0 -59581-1 0 00002
2 65364 53.1590 171.4176 0014761 155.2532 204.9179 15.28322182 04
| Epoch (UTC): | 25 May 2026 11:37:53 |
| Eccentricity: | 0.0014761 |
| inclination: | 53.1590° |
| perigee height: | 471 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 171.4176° |
| argument of perigee: | 155.2532° |
| revolutions per day: | 15.28322182 |
| mean anomaly at epoch: | 204.9179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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