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 00029U 60002B 25188.78996104 .00000277 00000-0 67021-4 0 9993
2 00029 48.3770 220.4987 0022875 226.9982 132.9015 14.78047587491170
Epoch (UTC): | 07 July 2025 18:57:32 |
Eccentricity: | 0.0022875 |
inclination: | 48.3770° |
perigee height: | 619 km |
apogee height: | 651 km |
right ascension of ascending node: | 220.4987° |
argument of perigee: | 226.9982° |
revolutions per day: | 14.78047587 |
mean anomaly at epoch: | 132.9015° |
orbit number at epoch: | 49117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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