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 60745U 26145.63484654 +.00000000 +00000-0 +10143-2 0 00004
2 60745 97.6700 286.1196 0008194 213.8801 146.1924 15.44564572 01
| Epoch (UTC): | 25 May 2026 15:14:10 |
| Eccentricity: | 0.0008194 |
| inclination: | 97.6700° |
| perigee height: | 427 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 286.1196° |
| argument of perigee: | 213.8801° |
| revolutions per day: | 15.44564572 |
| mean anomaly at epoch: | 146.1924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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