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 42778U 17036P 23086.84973402 .00024482 00000-0 72241-3 0 9990
2 42778 97.1688 123.7802 0009610 48.4045 311.8021 15.34932868320238
Epoch (UTC): | 27 March 2023 20:23:37 |
Eccentricity: | 0.0009610 |
inclination: | 97.1688° |
perigee height: | 454 km |
apogee height: | 467 km |
right ascension of ascending node: | 123.7802° |
argument of perigee: | 48.4045° |
revolutions per day: | 15.34932868 |
mean anomaly at epoch: | 311.8021° |
orbit number at epoch: | 32023 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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