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 59511U 26145.54255161 +.00000000 +00000-0 -18108-4 0 00004
2 59511 42.9998 243.6243 0001027 224.5070 135.5699 15.27590681 00
| Epoch (UTC): | 25 May 2026 13:01:16 |
| Eccentricity: | 0.0001027 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.6243° |
| argument of perigee: | 224.5070° |
| revolutions per day: | 15.27590681 |
| mean anomaly at epoch: | 135.5699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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