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 17997U 87043A 23069.78187572 0.00015500 00000-0 84221-3 0 04
2 17997 63.3371 309.2262 0913503 89.6999 270.3001 13.61555117 01
Epoch (UTC): | 10 March 2023 18:45:54 |
Eccentricity: | 0.0913503 |
inclination: | 63.3371° |
perigee height: | 353 km |
apogee height: | 1707 km |
right ascension of ascending node: | 309.2262° |
argument of perigee: | 89.6999° |
revolutions per day: | 13.61555117 |
mean anomaly at epoch: | 270.3001° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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