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 43941U 19004A 23155.99516449 0.00012000 00000-0 18483-3 0 01
2 43941 73.5581 100.8701 0015178 313.4124 46.5876 15.53928631 08
Epoch (UTC): | 04 June 2023 23:53:02 |
Eccentricity: | 0.0015178 |
inclination: | 73.5581° |
perigee height: | 395 km |
apogee height: | 415 km |
right ascension of ascending node: | 100.8701° |
argument of perigee: | 313.4124° |
revolutions per day: | 15.53928631 |
mean anomaly at epoch: | 46.5876° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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