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 59384U 26145.57093947 +.00000000 +00000-0 +33999-4 0 00001
2 59384 53.1607 258.4635 0001197 80.3772 279.7364 15.30186220 07
| Epoch (UTC): | 25 May 2026 13:42:09 |
| Eccentricity: | 0.0001197 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 258.4635° |
| argument of perigee: | 80.3772° |
| revolutions per day: | 15.30186220 |
| mean anomaly at epoch: | 279.7364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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