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 31701U 07027A 23265.12677628 0.00000000 00000-0 00000-0 0 08
2 31701 63.3867 2.8221 0377427 21.5990 338.4010 13.40867343 06
Epoch (UTC): | 22 September 2023 03:02:33 |
Eccentricity: | 0.0377427 |
inclination: | 63.3867° |
perigee height: | 823 km |
apogee height: | 1388 km |
right ascension of ascending node: | 2.8221° |
argument of perigee: | 21.5990° |
revolutions per day: | 13.40867343 |
mean anomaly at epoch: | 338.4010° |
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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