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 65027U 26145.49156963 +.00000000 +00000-0 +21483-2 0 00004
2 65027 53.1598 297.8104 0001200 170.2655 189.8369 15.30146454 00
| Epoch (UTC): | 25 May 2026 11:47:51 |
| Eccentricity: | 0.0001200 |
| inclination: | 53.1598° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 297.8104° |
| argument of perigee: | 170.2655° |
| revolutions per day: | 15.30146454 |
| mean anomaly at epoch: | 189.8369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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