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 59929U 26145.35542453 +.00000000 +00000-0 +49266-2 0 00005
2 59929 42.9930 256.3537 0002463 303.7757 56.2860 15.27604813 05
| Epoch (UTC): | 25 May 2026 08:31:48 |
| Eccentricity: | 0.0002463 |
| inclination: | 42.9930° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 256.3537° |
| argument of perigee: | 303.7757° |
| revolutions per day: | 15.27604813 |
| mean anomaly at epoch: | 56.2860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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