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 23087.80346629 -.00000123 00000-0 -38410-3 0 9998
2 00053 47.2801 10.7985 0097759 199.2040 160.5051 12.17292817792123
| Epoch (UTC): | 28 March 2023 19:16:59 |
| Eccentricity: | 0.0097759 |
| inclination: | 47.2801° |
| perigee height: | 1526 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 10.7985° |
| argument of perigee: | 199.2040° |
| revolutions per day: | 12.17292817 |
| mean anomaly at epoch: | 160.5051° |
| orbit number at epoch: | 79212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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