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 08027U 26022.41382086 +.00000000 +00000-0 +12004-3 0 00004
2 08027 81.2922 269.3774 0060620 64.5085 296.2338 14.07736337 07
| Epoch (UTC): | 22 January 2026 09:55:54 |
| Eccentricity: | 0.0060620 |
| inclination: | 81.2922° |
| perigee height: | 823 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 269.3774° |
| argument of perigee: | 64.5085° |
| revolutions per day: | 14.07736337 |
| mean anomaly at epoch: | 296.2338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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