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 33493U 09002B 23090.49833630 .00019662 00000-0 13976-2 0 9995
2 33493 98.2511 99.6637 0015093 310.6708 49.3204 15.04636740772063
Epoch (UTC): | 31 March 2023 11:57:36 |
Eccentricity: | 0.0015093 |
inclination: | 98.2511° |
perigee height: | 542 km |
apogee height: | 563 km |
right ascension of ascending node: | 99.6637° |
argument of perigee: | 310.6708° |
revolutions per day: | 15.04636740 |
mean anomaly at epoch: | 49.3204° |
orbit number at epoch: | 77206 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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