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 40057U 14034E 23091.14486186 .00006817 00000-0 88128-3 0 9993
2 40057 98.3733 280.7252 0010980 128.2618 231.9561 14.81220673472029
| Epoch (UTC): | 01 April 2023 03:28:36 |
| Eccentricity: | 0.0010980 |
| inclination: | 98.3733° |
| perigee height: | 618 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 280.7252° |
| argument of perigee: | 128.2618° |
| revolutions per day: | 14.81220673 |
| mean anomaly at epoch: | 231.9561° |
| orbit number at epoch: | 47202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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