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 19070U 88033A 23083.78089587 .00000169 00000-0 32161-3 0 9999
2 19070 90.3288 345.6901 0191621 64.5399 359.4305 13.27561841690645
| Epoch (UTC): | 24 March 2023 18:44:29 |
| Eccentricity: | 0.0191621 |
| inclination: | 90.3288° |
| perigee height: | 1011 km |
| apogee height: | 1300 km |
| right ascension of ascending node: | 345.6901° |
| argument of perigee: | 64.5399° |
| revolutions per day: | 13.27561841 |
| mean anomaly at epoch: | 359.4305° |
| orbit number at epoch: | 69064 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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