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 59216U 26145.35745205 +.00000000 +00000-0 +82319-4 0 00002
2 59216 53.1591 159.5140 0001286 76.9238 283.1907 15.30185580 02
| Epoch (UTC): | 25 May 2026 08:34:43 |
| Eccentricity: | 0.0001286 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 159.5140° |
| argument of perigee: | 76.9238° |
| revolutions per day: | 15.30185580 |
| mean anomaly at epoch: | 283.1907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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