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 60430U 26145.58391796 +.00000000 +00000-0 +24501-4 0 00008
2 60430 53.1609 219.1423 0001010 100.8167 259.2949 15.34384081 03
| Epoch (UTC): | 25 May 2026 14:00:50 |
| Eccentricity: | 0.0001010 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.1423° |
| argument of perigee: | 100.8167° |
| revolutions per day: | 15.34384081 |
| mean anomaly at epoch: | 259.2949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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