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 23079.11669745 .00009206 00000-0 44884-3 0 9998
2 40908 97.5263 82.4984 0016009 134.5952 294.3538 15.18433183414274
Epoch (UTC): | 20 March 2023 02:48:02 |
Eccentricity: | 0.0016009 |
inclination: | 97.5263° |
perigee height: | 499 km |
apogee height: | 521 km |
right ascension of ascending node: | 82.4984° |
argument of perigee: | 134.5952° |
revolutions per day: | 15.18433183 |
mean anomaly at epoch: | 294.3538° |
orbit number at epoch: | 41427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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