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 60145U 26145.66668980 +.00000000 +00000-0 -39054-3 0 00001
2 60145 53.1603 322.3562 0000897 75.4899 223.8058 15.33553884 08
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000897 |
| inclination: | 53.1603° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 322.3562° |
| argument of perigee: | 75.4899° |
| revolutions per day: | 15.33553884 |
| mean anomaly at epoch: | 223.8058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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