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 45074C 20006AG 25201.48798611 .00005988 00000+0 40136-3 0 2014
2 45074 53.0524 229.0152 0001190 79.7112 85.2873 15.06379682 11
Epoch (UTC): | 20 July 2025 11:42:42 |
Eccentricity: | 0.0001190 |
inclination: | 53.0524° |
perigee height: | 546 km |
apogee height: | 548 km |
right ascension of ascending node: | 229.0152° |
argument of perigee: | 79.7112° |
revolutions per day: | 15.06379682 |
mean anomaly at epoch: | 85.2873° |
orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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