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 59730U 26145.27861662 +.00000000 +00000-0 +95367-5 0 00008
2 59730 43.0028 110.9407 0000702 271.6400 88.4372 15.27575230 03
| Epoch (UTC): | 25 May 2026 06:41:12 |
| Eccentricity: | 0.0000702 |
| inclination: | 43.0028° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.9407° |
| argument of perigee: | 271.6400° |
| revolutions per day: | 15.27575230 |
| mean anomaly at epoch: | 88.4372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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