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 40016U 14033G 23273.46634854 .00001185 00000-0 17428-3 0 9999
2 40016 97.6476 87.6774 0048621 56.7189 303.8666 14.76391569499744
| Epoch (UTC): | 30 September 2023 11:11:32 |
| Eccentricity: | 0.0048621 |
| inclination: | 97.6476° |
| perigee height: | 606 km |
| apogee height: | 675 km |
| right ascension of ascending node: | 87.6774° |
| argument of perigee: | 56.7189° |
| revolutions per day: | 14.76391569 |
| mean anomaly at epoch: | 303.8666° |
| orbit number at epoch: | 49974 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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