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 34115U 93036KL 24358.03254273 .00011092 00000-0 17692-2 0 9993
2 34115 74.0092 217.2294 0035048 133.4165 226.9934 14.71579029841966
Epoch (UTC): | 23 December 2024 00:46:51 |
Eccentricity: | 0.0035048 |
inclination: | 74.0092° |
perigee height: | 631 km |
apogee height: | 680 km |
right ascension of ascending node: | 217.2294° |
argument of perigee: | 133.4165° |
revolutions per day: | 14.71579029 |
mean anomaly at epoch: | 226.9934° |
orbit number at epoch: | 84196 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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