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 20805U 26159.48095632 +.00000000 +00000-0 -28714-4 0 00005
2 20805 82.9354 146.3455 0029358 233.2077 249.7132 13.76236125 01
| Epoch (UTC): | 08 June 2026 11:32:34 |
| Eccentricity: | 0.0029358 |
| inclination: | 82.9354° |
| perigee height: | 956 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 146.3455° |
| argument of perigee: | 233.2077° |
| revolutions per day: | 13.76236125 |
| mean anomaly at epoch: | 249.7132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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