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 60141U 26145.50544279 +.00000000 +00000-0 +41155-2 0 00007
2 60141 53.1595 323.3644 0003147 80.9987 279.1370 15.29920377 07
| Epoch (UTC): | 25 May 2026 12:07:50 |
| Eccentricity: | 0.0003147 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 323.3644° |
| argument of perigee: | 80.9987° |
| revolutions per day: | 15.29920377 |
| mean anomaly at epoch: | 279.1370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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