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 22228.35650708 -.00000025 00000-0 58057-3 0 9999
2 00053 47.2794 343.0058 0098839 254.4370 104.5490 12.17275902764789
| Epoch (UTC): | 16 August 2022 08:33:22 |
| Eccentricity: | 0.0098839 |
| inclination: | 47.2794° |
| perigee height: | 1525 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 343.0058° |
| argument of perigee: | 254.4370° |
| revolutions per day: | 12.17275902 |
| mean anomaly at epoch: | 104.5490° |
| orbit number at epoch: | 76478 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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