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 59960U 26145.21228416 +.00000000 +00000-0 +58006-4 0 00009
2 59960 53.1604 70.0045 0001752 98.7895 261.3304 15.30225092 05
| Epoch (UTC): | 25 May 2026 05:05:41 |
| Eccentricity: | 0.0001752 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 70.0045° |
| argument of perigee: | 98.7895° |
| revolutions per day: | 15.30225092 |
| mean anomaly at epoch: | 261.3304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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