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 59285U 26145.61805616 +.00000000 +00000-0 +74700-4 0 00005
2 59285 50.0115 298.5916 0005339 102.3028 257.8485 14.27980796 01
| Epoch (UTC): | 25 May 2026 14:50:00 |
| Eccentricity: | 0.0005339 |
| inclination: | 50.0115° |
| perigee height: | 795 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 298.5916° |
| argument of perigee: | 102.3028° |
| revolutions per day: | 14.27980796 |
| mean anomaly at epoch: | 257.8485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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