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 59002U 26145.52257995 +.00000000 +00000-0 +52503-4 0 00000
2 59002 53.1607 81.4662 0000978 99.8655 260.2456 15.30190950 01
| Epoch (UTC): | 25 May 2026 12:32:30 |
| Eccentricity: | 0.0000978 |
| inclination: | 53.1607° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.4662° |
| argument of perigee: | 99.8655° |
| revolutions per day: | 15.30190950 |
| mean anomaly at epoch: | 260.2456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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