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 20804U 26053.80789528 +.00000000 +00000-0 +38413-4 0 00003
2 20804 82.9350 252.5154 0035732 236.1432 144.2906 13.74556066 07
| Epoch (UTC): | 22 February 2026 19:23:22 |
| Eccentricity: | 0.0035732 |
| inclination: | 82.9350° |
| perigee height: | 957 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 252.5154° |
| argument of perigee: | 236.1432° |
| revolutions per day: | 13.74556066 |
| mean anomaly at epoch: | 144.2906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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