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 3757U 68091AU 25119.18041252 .00023601 00000-0 33076-2 0 9990
2 3757 61.9814 95.8567 0368865 319.3040 38.0981 14.40163792773631
Epoch (UTC): | 29 April 2025 04:19:47 |
Eccentricity: | 0.0368865 |
inclination: | 61.9814° |
perigee height: | 495 km |
apogee height: | 1021 km |
right ascension of ascending node: | 95.8567° |
argument of perigee: | 319.3040° |
revolutions per day: | 14.40163792 |
mean anomaly at epoch: | 38.0981° |
orbit number at epoch: | 77363 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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