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 60151U 26145.47367370 +.00000000 +00000-0 -96095-6 0 00007
2 60151 53.1604 323.1616 0001206 91.5014 268.6125 15.30190135 03
| Epoch (UTC): | 25 May 2026 11:22:05 |
| Eccentricity: | 0.0001206 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 323.1616° |
| argument of perigee: | 91.5014° |
| revolutions per day: | 15.30190135 |
| mean anomaly at epoch: | 268.6125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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