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 23087.62987701 .00010207 00000-0 49485-3 0 9993
2 40908 97.5266 90.9720 0016174 108.2711 29.4720 15.18595756415561
Epoch (UTC): | 28 March 2023 15:07:01 |
Eccentricity: | 0.0016174 |
inclination: | 97.5266° |
perigee height: | 499 km |
apogee height: | 521 km |
right ascension of ascending node: | 90.9720° |
argument of perigee: | 108.2711° |
revolutions per day: | 15.18595756 |
mean anomaly at epoch: | 29.4720° |
orbit number at epoch: | 41556 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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