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 26088.15778310 +.00000000 +00000-0 +13081-3 0 00001
2 08800 81.2525 336.5549 0095256 103.3265 257.8549 14.10654789 08
| Epoch (UTC): | 29 March 2026 03:47:12 |
| Eccentricity: | 0.0095256 |
| inclination: | 81.2525° |
| perigee height: | 788 km |
| apogee height: | 926 km |
| right ascension of ascending node: | 336.5549° |
| argument of perigee: | 103.3265° |
| revolutions per day: | 14.10654789 |
| mean anomaly at epoch: | 257.8549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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