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 42790U 17036AB 23156.56127287 .16200993 23867-5 30465-3 0 9996
2 42790 97.1143 205.4465 0017814 252.9398 106.9954 16.45933448331901
Epoch (UTC): | 05 June 2023 13:28:13 |
Eccentricity: | 0.0017814 |
inclination: | 97.1143° |
perigee height: | 138 km |
apogee height: | 162 km |
right ascension of ascending node: | 205.4465° |
argument of perigee: | 252.9398° |
revolutions per day: | 16.45933448 |
mean anomaly at epoch: | 106.9954° |
orbit number at epoch: | 33190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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