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 40071U 14037C 23081.27814068 .00002448 00000-0 31087-3 0 9997
2 40071 98.3727 328.3138 0008969 137.0221 223.1678 14.82642517470499
Epoch (UTC): | 22 March 2023 06:40:31 |
Eccentricity: | 0.0008969 |
inclination: | 98.3727° |
perigee height: | 615 km |
apogee height: | 627 km |
right ascension of ascending node: | 328.3138° |
argument of perigee: | 137.0221° |
revolutions per day: | 14.82642517 |
mean anomaly at epoch: | 223.1678° |
orbit number at epoch: | 47049 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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