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 31702U 07027B 25133.88119918 .00013711 00000-0 83582-3 0 9990
2 31702 63.3205 17.4777 0509191 37.5553 325.9964 14.41618474 52993
Epoch (UTC): | 13 May 2025 21:08:55 |
Eccentricity: | 0.0509191 |
inclination: | 63.3205° |
perigee height: | 390 km |
apogee height: | 1116 km |
right ascension of ascending node: | 17.4777° |
argument of perigee: | 37.5553° |
revolutions per day: | 14.41618474 |
mean anomaly at epoch: | 325.9964° |
orbit number at epoch: | 5299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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