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 60559U 26145.21932794 +.00000000 +00000-0 +38779-3 0 00000
2 60559 97.3841 229.0107 0003500 47.1423 313.0116 15.39523950 06
| Epoch (UTC): | 25 May 2026 05:15:49 |
| Eccentricity: | 0.0003500 |
| inclination: | 97.3841° |
| perigee height: | 445 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 229.0107° |
| argument of perigee: | 47.1423° |
| revolutions per day: | 15.39523950 |
| mean anomaly at epoch: | 313.0116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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