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 65690U 26144.99235900 +.00000000 +00000-0 +69047-3 0 00002
2 65690 53.1598 351.4130 0000289 92.4291 267.6743 15.30211970 06
| Epoch (UTC): | 24 May 2026 23:48:59 |
| Eccentricity: | 0.0000289 |
| inclination: | 53.1598° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 351.4130° |
| argument of perigee: | 92.4291° |
| revolutions per day: | 15.30211970 |
| mean anomaly at epoch: | 267.6743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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