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 00805U 26086.64809980 +.00000000 +00000-0 +50137-3 0 00001
2 00805 89.8589 330.2575 0031413 97.3940 263.0831 14.35811544 00
| Epoch (UTC): | 27 March 2026 15:33:15 |
| Eccentricity: | 0.0031413 |
| inclination: | 89.8589° |
| perigee height: | 750 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 330.2575° |
| argument of perigee: | 97.3940° |
| revolutions per day: | 14.35811544 |
| mean anomaly at epoch: | 263.0831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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