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 37169U 10048B 23156.53774778 .00013543 00000-0 32840-3 0 9990
2 37169 97.9944 2.9373 0005446 69.5892 290.5937 15.41186550705612
Epoch (UTC): | 05 June 2023 12:54:21 |
Eccentricity: | 0.0005446 |
inclination: | 97.9944° |
perigee height: | 439 km |
apogee height: | 446 km |
right ascension of ascending node: | 2.9373° |
argument of perigee: | 69.5892° |
revolutions per day: | 15.41186550 |
mean anomaly at epoch: | 290.5937° |
orbit number at epoch: | 70561 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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