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 60434U 26145.39271330 +.00000000 +00000-0 -86260-4 0 00003
2 60434 53.1607 220.0807 0001066 88.5189 271.5936 15.34397877 09
| Epoch (UTC): | 25 May 2026 09:25:30 |
| Eccentricity: | 0.0001066 |
| inclination: | 53.1607° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 220.0807° |
| argument of perigee: | 88.5189° |
| revolutions per day: | 15.34397877 |
| mean anomaly at epoch: | 271.5936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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