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 06393U 73015B 23032.37943347 .00000109 00000-0 59349-4 0 9991
2 06393 81.2571 127.2046 0057682 261.4126 98.0503 14.05099898555327
| Epoch (UTC): | 01 February 2023 09:06:23 |
| Eccentricity: | 0.0057682 |
| inclination: | 81.2571° |
| perigee height: | 834 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 127.2046° |
| argument of perigee: | 261.4126° |
| revolutions per day: | 14.05099898 |
| mean anomaly at epoch: | 98.0503° |
| orbit number at epoch: | 55532 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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