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 05678U 26133.37942252 +.00000000 +00000-0 +16997-4 0 00004
2 05678 69.9879 96.2514 0010260 237.6099 122.4003 13.74138228 09
| Epoch (UTC): | 13 May 2026 09:06:22 |
| Eccentricity: | 0.0010260 |
| inclination: | 69.9879° |
| perigee height: | 977 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 96.2514° |
| argument of perigee: | 237.6099° |
| revolutions per day: | 13.74138228 |
| mean anomaly at epoch: | 122.4003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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