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 00051U 60009C 23088.72672946 -.00000028 00000-0 54133-3 0 9995
2 00051 47.2122 86.3959 0109582 301.0532 57.9536 12.18297506787867
| Epoch (UTC): | 29 March 2023 17:26:29 |
| Eccentricity: | 0.0109582 |
| inclination: | 47.2122° |
| perigee height: | 1512 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 86.3959° |
| argument of perigee: | 301.0532° |
| revolutions per day: | 12.18297506 |
| mean anomaly at epoch: | 57.9536° |
| orbit number at epoch: | 78786 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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