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 19770U 89005B 23265.92113517 .00000403 00000-0 13850-3 0 9990
2 19770 74.0458 150.2804 0004435 8.8843 2.1733 14.39266646815479
| Epoch (UTC): | 22 September 2023 22:06:26 |
| Eccentricity: | 0.0004435 |
| inclination: | 74.0458° |
| perigee height: | 758 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 150.2804° |
| argument of perigee: | 8.8843° |
| revolutions per day: | 14.39266646 |
| mean anomaly at epoch: | 2.1733° |
| orbit number at epoch: | 81547 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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