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 59496U 26145.37320876 +.00000000 +00000-0 +99295-3 0 00007
2 59496 42.9968 266.6504 0001123 291.2072 68.8660 15.27592488 07
| Epoch (UTC): | 25 May 2026 08:57:25 |
| Eccentricity: | 0.0001123 |
| inclination: | 42.9968° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.6504° |
| argument of perigee: | 291.2072° |
| revolutions per day: | 15.27592488 |
| mean anomaly at epoch: | 68.8660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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