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 36230U 99025DVF 22183.40878451 .00000958 00000-0 96844-3 0 9998
2 36230 99.5784 248.0590 0232196 163.0606 197.8458 13.68542233446239
Epoch (UTC): | 02 July 2022 09:48:38 |
Eccentricity: | 0.0232196 |
inclination: | 99.5784° |
perigee height: | 833 km |
apogee height: | 1176 km |
right ascension of ascending node: | 248.0590° |
argument of perigee: | 163.0606° |
revolutions per day: | 13.68542233 |
mean anomaly at epoch: | 197.8458° |
orbit number at epoch: | 44623 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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