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 02674U 67011A 23083.51967193 .00010863 00000-0 15090-2 0 9996
2 02674 39.9207 190.1261 0255496 127.6533 234.7717 14.57698580916795
Epoch (UTC): | 24 March 2023 12:28:19 |
Eccentricity: | 0.0255496 |
inclination: | 39.9207° |
perigee height: | 520 km |
apogee height: | 881 km |
right ascension of ascending node: | 190.1261° |
argument of perigee: | 127.6533° |
revolutions per day: | 14.57698580 |
mean anomaly at epoch: | 234.7717° |
orbit number at epoch: | 91679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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