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 59382U 26144.60809742 +.00000000 +00000-0 +58168-4 0 00005
2 59382 53.1611 263.1139 0001250 79.4551 280.6590 15.30193193 05
| Epoch (UTC): | 24 May 2026 14:35:39 |
| Eccentricity: | 0.0001250 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 263.1139° |
| argument of perigee: | 79.4551° |
| revolutions per day: | 15.30193193 |
| mean anomaly at epoch: | 280.6590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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