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 00020U 26149.60831804 +.00000000 +00000-0 +16984-3 0 00008
2 00020 33.3539 333.8350 1638136 313.9677 33.6698 11.61956564 08
| Epoch (UTC): | 29 May 2026 14:35:58 |
| Eccentricity: | 0.1638136 |
| inclination: | 33.3539° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 333.8350° |
| argument of perigee: | 313.9677° |
| revolutions per day: | 11.61956564 |
| mean anomaly at epoch: | 33.6698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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