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 19420U 88074B 23083.86250833 .00000136 00000-0 22006-3 0 9997
2 19420 90.0162 18.2934 0093698 194.3867 228.3268 13.42349660693160
| Epoch (UTC): | 24 March 2023 20:42:00 |
| Eccentricity: | 0.0093698 |
| inclination: | 90.0162° |
| perigee height: | 1030 km |
| apogee height: | 1170 km |
| right ascension of ascending node: | 18.2934° |
| argument of perigee: | 194.3867° |
| revolutions per day: | 13.42349660 |
| mean anomaly at epoch: | 228.3268° |
| orbit number at epoch: | 69316 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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