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 60142U 26145.20797269 +.00000000 +00000-0 +16030-4 0 00000
2 60142 53.1611 324.3522 0000953 91.8122 268.2990 15.34387123 06
| Epoch (UTC): | 25 May 2026 04:59:28 |
| Eccentricity: | 0.0000953 |
| inclination: | 53.1611° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 324.3522° |
| argument of perigee: | 91.8122° |
| revolutions per day: | 15.34387123 |
| mean anomaly at epoch: | 268.2990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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