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 07272U 74024H 23158.39158362 -.00000011 00000-0 31768-4 0 9993
2 07272 74.0181 323.4028 0033137 188.8579 191.3672 12.50349152242184
Epoch (UTC): | 07 June 2023 09:23:52 |
Eccentricity: | 0.0033137 |
inclination: | 74.0181° |
perigee height: | 1437 km |
apogee height: | 1489 km |
right ascension of ascending node: | 323.4028° |
argument of perigee: | 188.8579° |
revolutions per day: | 12.50349152 |
mean anomaly at epoch: | 191.3672° |
orbit number at epoch: | 24218 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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