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 65219U 26143.34146747 +.00000000 +00000-0 +49552-3 0 00006
2 65219 53.1586 165.7160 0001036 80.3530 279.7588 15.30193504 05
| Epoch (UTC): | 23 May 2026 08:11:42 |
| Eccentricity: | 0.0001036 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 165.7160° |
| argument of perigee: | 80.3530° |
| revolutions per day: | 15.30193504 |
| mean anomaly at epoch: | 279.7588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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