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 59356U 26145.41916429 +.00000000 +00000-0 -47265-5 0 00005
2 59356 43.0011 186.8860 0001111 271.2568 88.8156 15.27575855 07
| Epoch (UTC): | 25 May 2026 10:03:35 |
| Eccentricity: | 0.0001111 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.8860° |
| argument of perigee: | 271.2568° |
| revolutions per day: | 15.27575855 |
| mean anomaly at epoch: | 88.8156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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