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 53U 60009E 23030.17349142 -.00000028 00000-0 56317-3 0 9998
2 53 47.2736 188.5348 0098986 29.4563 331.1756 12.17289054785101
| Epoch (UTC): | 30 January 2023 04:09:49 |
| Eccentricity: | 0.0098986 |
| inclination: | 47.2736° |
| perigee height: | 1525 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 188.5348° |
| argument of perigee: | 29.4563° |
| revolutions per day: | 12.17289054 |
| mean anomaly at epoch: | 331.1756° |
| orbit number at epoch: | 78510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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