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 26088.09670619 +.00000000 +00000-0 +27077-4 0 00007
2 20805 82.9396 199.3624 0031844 75.3469 97.9285 13.76229291 04
| Epoch (UTC): | 29 March 2026 02:19:15 |
| Eccentricity: | 0.0031844 |
| inclination: | 82.9396° |
| perigee height: | 954 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 199.3624° |
| argument of perigee: | 75.3469° |
| revolutions per day: | 13.76229291 |
| mean anomaly at epoch: | 97.9285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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