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 23080.66136796 -.00000008 00000-0 75658-3 0 9993
2 00053 47.2790 32.8237 0097758 178.2725 181.8417 12.17292641791251
| Epoch (UTC): | 21 March 2023 15:52:22 |
| Eccentricity: | 0.0097758 |
| inclination: | 47.2790° |
| perigee height: | 1526 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 32.8237° |
| argument of perigee: | 178.2725° |
| revolutions per day: | 12.17292641 |
| mean anomaly at epoch: | 181.8417° |
| orbit number at epoch: | 79125 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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