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 59733U 26145.35815381 +.00000000 +00000-0 -84948-4 0 00000
2 59733 43.0030 110.6788 0001532 274.6280 85.4396 15.27553496 02
| Epoch (UTC): | 25 May 2026 08:35:44 |
| Eccentricity: | 0.0001532 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.6788° |
| argument of perigee: | 274.6280° |
| revolutions per day: | 15.27553496 |
| mean anomaly at epoch: | 85.4396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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