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 40021U 14033M 23333.45002362 .00014905 00000-0 11558-2 0 9995
2 40021 98.0754 303.2497 0015822 64.2393 296.0461 15.01397259513958
Epoch (UTC): | 29 November 2023 10:48:02 |
Eccentricity: | 0.0015822 |
inclination: | 98.0754° |
perigee height: | 551 km |
apogee height: | 573 km |
right ascension of ascending node: | 303.2497° |
argument of perigee: | 64.2393° |
revolutions per day: | 15.01397259 |
mean anomaly at epoch: | 296.0461° |
orbit number at epoch: | 51395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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