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 00053U 60009E 23275.38712971 .00000047 00000-0 13053-2 0 9995
2 00053 47.2751 152.2671 0100728 33.1956 327.5101 12.17313049814974
| Epoch (UTC): | 02 October 2023 09:17:28 |
| Eccentricity: | 0.0100728 |
| inclination: | 47.2751° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 152.2671° |
| argument of perigee: | 33.1956° |
| revolutions per day: | 12.17313049 |
| mean anomaly at epoch: | 327.5101° |
| orbit number at epoch: | 81497 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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