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 60555U 26145.17949917 +.00000000 +00000-0 +25401-3 0 00004
2 60555 97.6655 224.1998 0007879 181.9566 178.1629 15.01332370 02
| Epoch (UTC): | 25 May 2026 04:18:28 |
| Eccentricity: | 0.0007879 |
| inclination: | 97.6655° |
| perigee height: | 557 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 224.1998° |
| argument of perigee: | 181.9566° |
| revolutions per day: | 15.01332370 |
| mean anomaly at epoch: | 178.1629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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