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 23153.75196654 .00003962 00000-0 50845-3 0 9990
2 40057 98.3718 346.1397 0008755 291.3155 68.7121 14.81817308481298
| Epoch (UTC): | 02 June 2023 18:02:49 |
| Eccentricity: | 0.0008755 |
| inclination: | 98.3718° |
| perigee height: | 617 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 346.1397° |
| argument of perigee: | 291.3155° |
| revolutions per day: | 14.81817308 |
| mean anomaly at epoch: | 68.7121° |
| orbit number at epoch: | 48129 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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