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 40908U 15049K 23335.20652276 .00010707 00000-0 46641-3 0 9995
2 40908 97.5276 338.1079 0012411 335.9915 24.0740 15.22322851453183
Epoch (UTC): | 01 December 2023 04:57:23 |
Eccentricity: | 0.0012411 |
inclination: | 97.5276° |
perigee height: | 490 km |
apogee height: | 507 km |
right ascension of ascending node: | 338.1079° |
argument of perigee: | 335.9915° |
revolutions per day: | 15.22322851 |
mean anomaly at epoch: | 24.0740° |
orbit number at epoch: | 45318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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