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 23333.05890098 .00000244 00000-0 13219-3 0 9996
2 40069 98.4284 331.4180 0005014 213.7749 146.3110 14.20848749487067
| Epoch (UTC): | 29 November 2023 01:24:49 |
| Eccentricity: | 0.0005014 |
| inclination: | 98.4284° |
| perigee height: | 819 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 331.4180° |
| argument of perigee: | 213.7749° |
| revolutions per day: | 14.20848749 |
| mean anomaly at epoch: | 146.3110° |
| orbit number at epoch: | 48706 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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