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 23079.16594366 .00221419 00000-0 88441-3 0 9993
2 40903 97.1281 146.1586 0006640 176.6000 262.4017 15.85982634422329
Epoch (UTC): | 20 March 2023 03:58:57 |
Eccentricity: | 0.0006640 |
inclination: | 97.1281° |
perigee height: | 309 km |
apogee height: | 318 km |
right ascension of ascending node: | 146.1586° |
argument of perigee: | 176.6000° |
revolutions per day: | 15.85982634 |
mean anomaly at epoch: | 262.4017° |
orbit number at epoch: | 42232 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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