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 59028U 26145.56915221 +.00000000 +00000-0 +67308-4 0 00004
2 59028 43.0005 247.8446 0001159 271.7984 88.2735 15.27575538 08
| Epoch (UTC): | 25 May 2026 13:39:34 |
| Eccentricity: | 0.0001159 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.8446° |
| argument of perigee: | 271.7984° |
| revolutions per day: | 15.27575538 |
| mean anomaly at epoch: | 88.2735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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