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 59864U 26145.52714236 +.00000000 +00000-0 +86007-6 0 00000
2 59864 42.9997 204.3858 0001171 274.6742 85.3976 15.27580208 02
| Epoch (UTC): | 25 May 2026 12:39:05 |
| Eccentricity: | 0.0001171 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.3858° |
| argument of perigee: | 274.6742° |
| revolutions per day: | 15.27580208 |
| mean anomaly at epoch: | 85.3976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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