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 39271U 13055G 23080.80111800 .00031625 00000-0 60374-3 0 9998
2 39271 80.9495 246.6600 0467390 335.7930 22.1923 14.78285999497508
| Epoch (UTC): | 21 March 2023 19:13:36 |
| Eccentricity: | 0.0467390 |
| inclination: | 80.9495° |
| perigee height: | 307 km |
| apogee height: | 962 km |
| right ascension of ascending node: | 246.6600° |
| argument of perigee: | 335.7930° |
| revolutions per day: | 14.78285999 |
| mean anomaly at epoch: | 22.1923° |
| orbit number at epoch: | 49750 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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