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 59099U 26145.37058334 +.00000000 +00000-0 +39389-3 0 00001
2 59099 97.8574 283.4973 0008210 60.5349 299.6697 15.08272463 04
| Epoch (UTC): | 25 May 2026 08:53:38 |
| Eccentricity: | 0.0008210 |
| inclination: | 97.8574° |
| perigee height: | 536 km |
| apogee height: | 547 km |
| right ascension of ascending node: | 283.4973° |
| argument of perigee: | 60.5349° |
| revolutions per day: | 15.08272463 |
| mean anomaly at epoch: | 299.6697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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