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 60261U 26145.16644561 +.00000000 +00000-0 +56466-4 0 00000
2 60261 53.1603 57.4760 0001201 77.7616 282.3519 15.30192937 02
| Epoch (UTC): | 25 May 2026 03:59:40 |
| Eccentricity: | 0.0001201 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.4760° |
| argument of perigee: | 77.7616° |
| revolutions per day: | 15.30192937 |
| mean anomaly at epoch: | 282.3519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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