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 42203U 81053TT 23025.96966815 .00001702 00000-0 18039-2 0 9993
2 42203 82.9965 93.0624 0118963 279.5593 254.2341 13.70853786458493
Epoch (UTC): | 25 January 2023 23:16:19 |
Eccentricity: | 0.0118963 |
inclination: | 82.9965° |
perigee height: | 909 km |
apogee height: | 1084 km |
right ascension of ascending node: | 93.0624° |
argument of perigee: | 279.5593° |
revolutions per day: | 13.70853786 |
mean anomaly at epoch: | 254.2341° |
orbit number at epoch: | 45849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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