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 41465U 16026B 23083.64942774 .00032244 00000-0 51131-3 0 9993
2 41465 97.0102 316.6387 0007702 173.4270 271.7931 15.53291328386821
Epoch (UTC): | 24 March 2023 15:35:10 |
Eccentricity: | 0.0007702 |
inclination: | 97.0102° |
perigee height: | 402 km |
apogee height: | 412 km |
right ascension of ascending node: | 316.6387° |
argument of perigee: | 173.4270° |
revolutions per day: | 15.53291328 |
mean anomaly at epoch: | 271.7931° |
orbit number at epoch: | 38682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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