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 40069U 14037A 23332.56595728 .00000268 00000-0 14326-3 0 9999
2 40069 98.4284 330.9478 0004986 215.3831 144.7017 14.20848504486996
| Epoch (UTC): | 28 November 2023 13:34:58 |
| Eccentricity: | 0.0004986 |
| inclination: | 98.4284° |
| perigee height: | 819 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 330.9478° |
| argument of perigee: | 215.3831° |
| revolutions per day: | 14.20848504 |
| mean anomaly at epoch: | 144.7017° |
| orbit number at epoch: | 48699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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