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 59885U 26145.43204801 +.00000000 +00000-0 -88219-5 0 00002
2 59885 43.0024 51.9983 0000551 316.8122 43.2686 15.27575490 03
| Epoch (UTC): | 25 May 2026 10:22:08 |
| Eccentricity: | 0.0000551 |
| inclination: | 43.0024° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 51.9983° |
| argument of perigee: | 316.8122° |
| revolutions per day: | 15.27575490 |
| mean anomaly at epoch: | 43.2686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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