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 39770U 14029E 23078.79156323 .00030969 00000-0 26190-2 0 9995
2 39770 97.9591 203.8000 0008963 245.8628 114.1621 14.97954288478756
Epoch (UTC): | 19 March 2023 18:59:51 |
Eccentricity: | 0.0008963 |
inclination: | 97.9591° |
perigee height: | 567 km |
apogee height: | 579 km |
right ascension of ascending node: | 203.8000° |
argument of perigee: | 245.8628° |
revolutions per day: | 14.97954288 |
mean anomaly at epoch: | 114.1621° |
orbit number at epoch: | 47875 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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