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 33410U 08053C 22142.04058202 .00004332 00000-0 29511-3 0 9992
2 33410 97.8985 148.2589 0125325 279.9261 78.7836 15.00610586740439
Epoch (UTC): | 22 May 2022 00:58:26 |
Eccentricity: | 0.0125325 |
inclination: | 97.8985° |
perigee height: | 478 km |
apogee height: | 652 km |
right ascension of ascending node: | 148.2589° |
argument of perigee: | 279.9261° |
revolutions per day: | 15.00610586 |
mean anomaly at epoch: | 78.7836° |
orbit number at epoch: | 74043 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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