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 66194U 26145.00384723 +.00000000 +00000-0 +50408-3 0 00004
2 66194 53.1601 250.3672 0001277 76.1263 283.9880 15.31709810 04
| Epoch (UTC): | 25 May 2026 00:05:32 |
| Eccentricity: | 0.0001277 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 250.3672° |
| argument of perigee: | 76.1263° |
| revolutions per day: | 15.31709810 |
| mean anomaly at epoch: | 283.9880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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