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 60580U 26145.43099264 +.00000000 +00000-0 +49196-3 0 00009
2 60580 97.6636 226.0085 0010182 71.8242 288.4093 15.06678791 01
| Epoch (UTC): | 25 May 2026 10:20:37 |
| Eccentricity: | 0.0010182 |
| inclination: | 97.6636° |
| perigee height: | 539 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 226.0085° |
| argument of perigee: | 71.8242° |
| revolutions per day: | 15.06678791 |
| mean anomaly at epoch: | 288.4093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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