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 59425U 26145.53423917 +.00000000 +00000-0 +47161-4 0 00003
2 59425 53.1577 74.9765 0001093 101.5962 258.5179 15.69704670 02
| Epoch (UTC): | 25 May 2026 12:49:18 |
| Eccentricity: | 0.0001093 |
| inclination: | 53.1577° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 74.9765° |
| argument of perigee: | 101.5962° |
| revolutions per day: | 15.69704670 |
| mean anomaly at epoch: | 258.5179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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