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 66967U 26145.48829384 +.00000000 +00000-0 +62347-3 0 00006
2 66967 42.9995 309.6584 0000841 281.7826 78.2931 15.27591922 09
| Epoch (UTC): | 25 May 2026 11:43:08 |
| Eccentricity: | 0.0000841 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.6584° |
| argument of perigee: | 281.7826° |
| revolutions per day: | 15.27591922 |
| mean anomaly at epoch: | 78.2931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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