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 60426U 26145.48713573 +.00000000 +00000-0 +24502-4 0 00004
2 60426 53.1598 220.6690 0001029 77.9475 282.1641 15.30192919 01
| Epoch (UTC): | 25 May 2026 11:41:28 |
| Eccentricity: | 0.0001029 |
| inclination: | 53.1598° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 220.6690° |
| argument of perigee: | 77.9475° |
| revolutions per day: | 15.30192919 |
| mean anomaly at epoch: | 282.1641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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