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 42778U 17036P 23334.63659408 .00053292 00000-0 94958-3 0 9990
2 42778 97.1322 6.4688 0005266 197.1886 162.9189 15.49927159358403
Epoch (UTC): | 30 November 2023 15:16:41 |
Eccentricity: | 0.0005266 |
inclination: | 97.1322° |
perigee height: | 413 km |
apogee height: | 420 km |
right ascension of ascending node: | 6.4688° |
argument of perigee: | 197.1886° |
revolutions per day: | 15.49927159 |
mean anomaly at epoch: | 162.9189° |
orbit number at epoch: | 35840 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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