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 59902U 26145.12309385 +.00000000 +00000-0 +93604-5 0 00004
2 59902 43.0029 53.9749 0001152 277.4561 82.6160 15.27582988 01
| Epoch (UTC): | 25 May 2026 02:57:15 |
| Eccentricity: | 0.0001152 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 53.9749° |
| argument of perigee: | 277.4561° |
| revolutions per day: | 15.27582988 |
| mean anomaly at epoch: | 82.6160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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