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 23084.70742215 -.00000104 00000-0 -19644-3 0 9990
2 00051 47.2116 98.8318 0109542 289.0648 69.8303 12.18297341787373
| Epoch (UTC): | 25 March 2023 16:58:41 |
| Eccentricity: | 0.0109542 |
| inclination: | 47.2116° |
| perigee height: | 1512 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 98.8318° |
| argument of perigee: | 289.0648° |
| revolutions per day: | 12.18297341 |
| mean anomaly at epoch: | 69.8303° |
| orbit number at epoch: | 78737 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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