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 08800U 26071.77313902 +.00000000 +00000-0 +53883-4 0 00008
2 08800 81.2543 352.5060 0094079 149.4110 211.2596 14.10651460 05
| Epoch (UTC): | 12 March 2026 18:33:19 |
| Eccentricity: | 0.0094079 |
| inclination: | 81.2543° |
| perigee height: | 789 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 352.5060° |
| argument of perigee: | 149.4110° |
| revolutions per day: | 14.10651460 |
| mean anomaly at epoch: | 211.2596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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