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 68187U 26144.75381014 +.00000000 +00000-0 +97472-3 0 00001
2 68187 53.1598 273.1005 0000973 87.0854 273.0260 15.34398319 08
| Epoch (UTC): | 24 May 2026 18:05:29 |
| Eccentricity: | 0.0000973 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 273.1005° |
| argument of perigee: | 87.0854° |
| revolutions per day: | 15.34398319 |
| mean anomaly at epoch: | 273.0260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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