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 23342.57562014 .00029831 00000-0 52052-3 0 9999
2 42778 97.1331 14.3281 0006228 168.4871 191.6525 15.50636789359631
Epoch (UTC): | 08 December 2023 13:48:53 |
Eccentricity: | 0.0006228 |
inclination: | 97.1331° |
perigee height: | 410 km |
apogee height: | 419 km |
right ascension of ascending node: | 14.3281° |
argument of perigee: | 168.4871° |
revolutions per day: | 15.50636789 |
mean anomaly at epoch: | 191.6525° |
orbit number at epoch: | 35963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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