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 59135U 26145.01661800 +.00000000 +00000-0 +10331-5 0 00009
2 59135 97.5395 281.1914 0008240 328.0146 32.0591 15.26618389 06
| Epoch (UTC): | 25 May 2026 00:23:55 |
| Eccentricity: | 0.0008240 |
| inclination: | 97.5395° |
| perigee height: | 480 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 281.1914° |
| argument of perigee: | 328.0146° |
| revolutions per day: | 15.26618389 |
| mean anomaly at epoch: | 32.0591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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