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 20442U 90005G 23081.81386597 .00000367 00000-0 15011-3 0 9994
2 20442 98.8358 56.5254 0012836 73.4911 286.7682 14.33203889733033
| Epoch (UTC): | 22 March 2023 19:31:58 |
| Eccentricity: | 0.0012836 |
| inclination: | 98.8358° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 56.5254° |
| argument of perigee: | 73.4911° |
| revolutions per day: | 14.33203889 |
| mean anomaly at epoch: | 286.7682° |
| orbit number at epoch: | 73303 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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