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 55068U 23001BM 23271.10128971 .00011768 00000-0 54405-3 0 9998
2 55068 97.4657 329.8453 0014258 15.4450 344.7217 15.20230131 40715
Epoch (UTC): | 28 September 2023 02:25:51 |
Eccentricity: | 0.0014258 |
inclination: | 97.4657° |
perigee height: | 495 km |
apogee height: | 515 km |
right ascension of ascending node: | 329.8453° |
argument of perigee: | 15.4450° |
revolutions per day: | 15.20230131 |
mean anomaly at epoch: | 344.7217° |
orbit number at epoch: | 4071 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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