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 33499U 09002H 23078.83195071 .00002146 00000-0 31377-3 0 9990
2 33499 98.1846 329.9717 0009410 146.0657 214.1156 14.76746283760873
Epoch (UTC): | 19 March 2023 19:58:00 |
Eccentricity: | 0.0009410 |
inclination: | 98.1846° |
perigee height: | 633 km |
apogee height: | 646 km |
right ascension of ascending node: | 329.9717° |
argument of perigee: | 146.0657° |
revolutions per day: | 14.76746283 |
mean anomaly at epoch: | 214.1156° |
orbit number at epoch: | 76087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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