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 08026U 26121.88579278 +.00000000 +00000-0 +11243-3 0 00009
2 08026 81.2791 68.2079 0021870 355.0836 5.0117 14.10802736 02
| Epoch (UTC): | 01 May 2026 21:15:32 |
| Eccentricity: | 0.0021870 |
| inclination: | 81.2791° |
| perigee height: | 841 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 68.2079° |
| argument of perigee: | 355.0836° |
| revolutions per day: | 14.10802736 |
| mean anomaly at epoch: | 5.0117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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