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 60552U 26145.15779875 +.00000000 +00000-0 +19925-3 0 00007
2 60552 97.6823 222.2095 0006226 146.3547 213.8072 14.97942369 00
| Epoch (UTC): | 25 May 2026 03:47:13 |
| Eccentricity: | 0.0006226 |
| inclination: | 97.6823° |
| perigee height: | 569 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 222.2095° |
| argument of perigee: | 146.3547° |
| revolutions per day: | 14.97942369 |
| mean anomaly at epoch: | 213.8072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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