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 43803U 18099AX 25166.90056614 .00009141 00000-0 41506-3 0 9990
2 43803 97.4651 225.9203 0009080 119.7599 240.4541 15.20973998357731
Epoch (UTC): | 15 June 2025 21:36:48 |
Eccentricity: | 0.0009080 |
inclination: | 97.4651° |
perigee height: | 496 km |
apogee height: | 509 km |
right ascension of ascending node: | 225.9203° |
argument of perigee: | 119.7599° |
revolutions per day: | 15.20973998 |
mean anomaly at epoch: | 240.4541° |
orbit number at epoch: | 35773 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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