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 23087.16904133 .00312944 38123-4 10251-2 0 9997
2 40903 97.1221 154.5325 0005481 161.5498 283.1052 15.90545002423592
Epoch (UTC): | 28 March 2023 04:03:25 |
Eccentricity: | 0.0005481 |
inclination: | 97.1221° |
perigee height: | 297 km |
apogee height: | 304 km |
right ascension of ascending node: | 154.5325° |
argument of perigee: | 161.5498° |
revolutions per day: | 15.90545002 |
mean anomaly at epoch: | 283.1052° |
orbit number at epoch: | 42359 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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