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 26074.25566876 +.00000000 +00000-0 +26067-4 0 00008
2 08800 81.2541 350.0893 0094199 142.4319 218.3485 14.10651694 01
| Epoch (UTC): | 15 March 2026 06:08:09 |
| Eccentricity: | 0.0094199 |
| inclination: | 81.2541° |
| perigee height: | 789 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 350.0893° |
| argument of perigee: | 142.4319° |
| revolutions per day: | 14.10651694 |
| mean anomaly at epoch: | 218.3485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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