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 60373U 26145.61118039 +.00000000 +00000-0 +22083-2 0 00006
2 60373 53.1597 312.3766 0001859 97.9936 262.1276 15.30722980 08
| Epoch (UTC): | 25 May 2026 14:40:05 |
| Eccentricity: | 0.0001859 |
| inclination: | 53.1597° |
| perigee height: | 472 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 312.3766° |
| argument of perigee: | 97.9936° |
| revolutions per day: | 15.30722980 |
| mean anomaly at epoch: | 262.1276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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