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 23335.09855084 .00006891 00000-0 84212-3 0 9997
2 40057 98.3576 175.8029 0010707 66.9074 293.3266 14.83570168508169
| Epoch (UTC): | 01 December 2023 02:21:54 |
| Eccentricity: | 0.0010707 |
| inclination: | 98.3576° |
| perigee height: | 610 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 175.8029° |
| argument of perigee: | 66.9074° |
| revolutions per day: | 14.83570168 |
| mean anomaly at epoch: | 293.3266° |
| orbit number at epoch: | 50816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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