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 60260U 26145.17583508 +.00000000 +00000-0 -44363-4 0 00007
2 60260 53.1604 56.8351 0001159 78.1742 281.9389 15.30188758 04
| Epoch (UTC): | 25 May 2026 04:13:12 |
| Eccentricity: | 0.0001159 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 56.8351° |
| argument of perigee: | 78.1742° |
| revolutions per day: | 15.30188758 |
| mean anomaly at epoch: | 281.9389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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