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 25192.93498243 0.00000000 00000-0 00000-0 0 02
2 31701 63.3937 117.2458 0457432 22.7495 337.2218 13.40966554 06
Epoch (UTC): | 11 July 2025 22:26:22 |
Eccentricity: | 0.0457432 |
inclination: | 63.3937° |
perigee height: | 763 km |
apogee height: | 1448 km |
right ascension of ascending node: | 117.2458° |
argument of perigee: | 22.7495° |
revolutions per day: | 13.40966554 |
mean anomaly at epoch: | 337.2218° |
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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