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 30776U 07006E 22180.33919209 .00021533 00000-0 32039-3 0 9999
2 30776 35.4290 182.3612 0003966 212.0469 148.0022 15.54197832851432
Epoch (UTC): | 29 June 2022 08:08:26 |
Eccentricity: | 0.0003966 |
inclination: | 35.4290° |
perigee height: | 402 km |
apogee height: | 407 km |
right ascension of ascending node: | 182.3612° |
argument of perigee: | 212.0469° |
revolutions per day: | 15.54197832 |
mean anomaly at epoch: | 148.0022° |
orbit number at epoch: | 85143 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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