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 19822U 89016A 23333.05488251 .00169574 43596-5 15411-2 0 9991
2 19822 74.9480 188.0651 1012570 302.0565 48.6072 13.73530330198106
| Epoch (UTC): | 29 November 2023 01:19:01 |
| Eccentricity: | 0.1012570 |
| inclination: | 74.9480° |
| perigee height: | 241 km |
| apogee height: | 1732 km |
| right ascension of ascending node: | 188.0651° |
| argument of perigee: | 302.0565° |
| revolutions per day: | 13.73530330 |
| mean anomaly at epoch: | 48.6072° |
| orbit number at epoch: | 19810 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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