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 59901U 26145.42272624 +.00000000 +00000-0 -13788-4 0 00006
2 59901 42.9974 45.0027 0001540 281.0201 79.0477 15.27582327 09
| Epoch (UTC): | 25 May 2026 10:08:43 |
| Eccentricity: | 0.0001540 |
| inclination: | 42.9974° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 45.0027° |
| argument of perigee: | 281.0201° |
| revolutions per day: | 15.27582327 |
| mean anomaly at epoch: | 79.0477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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