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 59890U 26145.02430272 +.00000000 +00000-0 +35816-4 0 00009
2 59890 43.0022 54.0934 0001282 253.4296 106.6415 15.27583311 02
| Epoch (UTC): | 25 May 2026 00:34:59 |
| Eccentricity: | 0.0001282 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 54.0934° |
| argument of perigee: | 253.4296° |
| revolutions per day: | 15.27583311 |
| mean anomaly at epoch: | 106.6415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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