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 59626U 26145.62567951 +.00000000 +00000-0 +20895-3 0 00007
2 59626 97.5018 223.8244 0012783 59.8460 300.4037 15.16459175 09
| Epoch (UTC): | 25 May 2026 15:00:58 |
| Eccentricity: | 0.0012783 |
| inclination: | 97.5018° |
| perigee height: | 508 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 223.8244° |
| argument of perigee: | 59.8460° |
| revolutions per day: | 15.16459175 |
| mean anomaly at epoch: | 300.4037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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