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 60091U 26145.40860238 +.00000000 +00000-0 +10374-3 0 00006
2 60091 53.1586 40.6877 0001085 56.7855 303.3250 15.30188684 08
| Epoch (UTC): | 25 May 2026 09:48:23 |
| Eccentricity: | 0.0001085 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.6877° |
| argument of perigee: | 56.7855° |
| revolutions per day: | 15.30188684 |
| mean anomaly at epoch: | 303.3250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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