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 23331.04565618 -.00000152 00000-0 -66610-3 0 9992
2 00053 47.2789 340.6019 0099816 198.7709 160.9386 12.17317498821753
| Epoch (UTC): | 27 November 2023 01:05:44 |
| Eccentricity: | 0.0099816 |
| inclination: | 47.2789° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 340.6019° |
| argument of perigee: | 198.7709° |
| revolutions per day: | 12.17317498 |
| mean anomaly at epoch: | 160.9386° |
| orbit number at epoch: | 82175 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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