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 59223U 26145.41747631 +.00000000 +00000-0 -49666-4 0 00001
2 59223 53.1593 159.1708 0001281 91.6052 268.5095 15.30179739 05
| Epoch (UTC): | 25 May 2026 10:01:09 |
| Eccentricity: | 0.0001281 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 159.1708° |
| argument of perigee: | 91.6052° |
| revolutions per day: | 15.30179739 |
| mean anomaly at epoch: | 268.5095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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