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 42834U 17042K 23332.06639104 .00005339 00000-0 48480-3 0 9994
2 42834 97.3779 161.2199 0013069 39.5083 320.7090 14.95600689347037
Epoch (UTC): | 28 November 2023 01:35:36 |
Eccentricity: | 0.0013069 |
inclination: | 97.3779° |
perigee height: | 571 km |
apogee height: | 589 km |
right ascension of ascending node: | 161.2199° |
argument of perigee: | 39.5083° |
revolutions per day: | 14.95600689 |
mean anomaly at epoch: | 320.7090° |
orbit number at epoch: | 34703 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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