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 data is extracted from the following two-line orbital elements,
1 20441U 90005F 23081.83266793 .00000367 00000-0 15075-3 0 9990
2 20441 98.8582 62.5332 0012585 86.2901 338.0601 14.33095705732887
| Epoch (UTC): | 22 March 2023 19:59:02 |
| Eccentricity: | 0.0012585 |
| inclination: | 98.8582° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 62.5332° |
| argument of perigee: | 86.2901° |
| revolutions per day: | 14.33095705 |
| mean anomaly at epoch: | 338.0601° |
| orbit number at epoch: | 73288 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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