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 59024U 26145.34170667 +.00000000 +00000-0 +22906-3 0 00007
2 59024 43.0007 263.7216 0000906 256.9618 103.1133 15.27570171 03
| Epoch (UTC): | 25 May 2026 08:12:03 |
| Eccentricity: | 0.0000906 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 263.7216° |
| argument of perigee: | 256.9618° |
| revolutions per day: | 15.27570171 |
| mean anomaly at epoch: | 103.1133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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