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 40903U 15049E 22176.45522601 .00020476 00000-0 31910-3 0 9994
2 40903 97.1785 234.9992 0011284 93.2318 27.8392 15.53822026380506
Epoch (UTC): | 25 June 2022 10:55:31 |
Eccentricity: | 0.0011284 |
inclination: | 97.1785° |
perigee height: | 398 km |
apogee height: | 413 km |
right ascension of ascending node: | 234.9992° |
argument of perigee: | 93.2318° |
revolutions per day: | 15.53822026 |
mean anomaly at epoch: | 27.8392° |
orbit number at epoch: | 38050 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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