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 60266U 26145.50003470 +.00000000 +00000-0 +43893-3 0 00000
2 60266 53.1609 55.8346 0001236 97.5743 355.1226 15.31689950 05
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001236 |
| inclination: | 53.1609° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 55.8346° |
| argument of perigee: | 97.5743° |
| revolutions per day: | 15.31689950 |
| mean anomaly at epoch: | 355.1226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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