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 60551U 26145.45620466 +.00000000 +00000-0 +26989-4 0 00009
2 60551 97.6877 221.6426 0007018 162.2359 197.9109 14.96125699 08
| Epoch (UTC): | 25 May 2026 10:56:56 |
| Eccentricity: | 0.0007018 |
| inclination: | 97.6877° |
| perigee height: | 574 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 221.6426° |
| argument of perigee: | 162.2359° |
| revolutions per day: | 14.96125699 |
| mean anomaly at epoch: | 197.9109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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