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 29873U 99025FT 23340.50543154 .00000116 00000-0 11323-3 0 9994
2 29873 99.4999 166.0430 0094308 36.8576 18.3675 13.96869991860172
Epoch (UTC): | 06 December 2023 12:07:49 |
Eccentricity: | 0.0094308 |
inclination: | 99.4999° |
perigee height: | 836 km |
apogee height: | 973 km |
right ascension of ascending node: | 166.0430° |
argument of perigee: | 36.8576° |
revolutions per day: | 13.96869991 |
mean anomaly at epoch: | 18.3675° |
orbit number at epoch: | 86017 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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