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 59886U 26145.43461686 +.00000000 +00000-0 -33753-4 0 00001
2 59886 43.0033 52.0161 0000396 322.0130 38.0694 15.27581196 00
| Epoch (UTC): | 25 May 2026 10:25:50 |
| Eccentricity: | 0.0000396 |
| inclination: | 43.0033° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 52.0161° |
| argument of perigee: | 322.0130° |
| revolutions per day: | 15.27581196 |
| mean anomaly at epoch: | 38.0694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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