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 59141U 26145.38389623 +.00000000 +00000-0 +24929-3 0 00002
2 59141 97.5458 295.3586 0004800 248.6750 111.3988 15.47943534 08
| Epoch (UTC): | 25 May 2026 09:12:48 |
| Eccentricity: | 0.0004800 |
| inclination: | 97.5458° |
| perigee height: | 419 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 295.3586° |
| argument of perigee: | 248.6750° |
| revolutions per day: | 15.47943534 |
| mean anomaly at epoch: | 111.3988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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