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 57217U 23091AV 24358.22869702 .00017746 00000-0 95221-3 0 9992
2 57217 97.5871 49.5173 0015152 183.6751 176.4372 15.14911725 82067
Epoch (UTC): | 23 December 2024 05:29:19 |
Eccentricity: | 0.0015152 |
inclination: | 97.5871° |
perigee height: | 511 km |
apogee height: | 532 km |
right ascension of ascending node: | 49.5173° |
argument of perigee: | 183.6751° |
revolutions per day: | 15.14911725 |
mean anomaly at epoch: | 176.4372° |
orbit number at epoch: | 8206 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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