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 60350U 26145.52560242 +.00000000 +00000-0 -13714-4 0 00002
2 60350 53.1613 78.4001 0001253 90.2972 269.8173 15.31701179 06
| Epoch (UTC): | 25 May 2026 12:36:52 |
| Eccentricity: | 0.0001253 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 78.4001° |
| argument of perigee: | 90.2972° |
| revolutions per day: | 15.31701179 |
| mean anomaly at epoch: | 269.8173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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