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 23343.93403901 -.00000031 00000-0 52101-3 0 9994
2 00053 47.2790 300.8519 0099406 236.9128 122.2085 12.17318486823323
| Epoch (UTC): | 09 December 2023 22:25:00 |
| Eccentricity: | 0.0099406 |
| inclination: | 47.2790° |
| perigee height: | 1525 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 300.8519° |
| argument of perigee: | 236.9128° |
| revolutions per day: | 12.17318486 |
| mean anomaly at epoch: | 122.2085° |
| orbit number at epoch: | 82332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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