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 40034U 14033AA 25118.86734054 .00006303 00000-0 69902-3 0 9997
2 40034 97.7306 278.2950 0046217 346.6911 13.3083 14.86827116584164
Epoch (UTC): | 28 April 2025 20:48:58 |
Eccentricity: | 0.0046217 |
inclination: | 97.7306° |
perigee height: | 575 km |
apogee height: | 640 km |
right ascension of ascending node: | 278.2950° |
argument of perigee: | 346.6911° |
revolutions per day: | 14.86827116 |
mean anomaly at epoch: | 13.3083° |
orbit number at epoch: | 58416 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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