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 59209U 26145.41587963 +.00000000 +00000-0 +47662-4 0 00008
2 59209 53.1603 157.7530 0001200 90.1163 269.9977 15.34388007 04
| Epoch (UTC): | 25 May 2026 09:58:52 |
| Eccentricity: | 0.0001200 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 157.7530° |
| argument of perigee: | 90.1163° |
| revolutions per day: | 15.34388007 |
| mean anomaly at epoch: | 269.9977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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