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 40012U 14033C 23090.53383389 .00004773 00000-0 67883-3 0 9990
2 40012 97.6685 268.4523 0054994 309.0794 50.5531 14.76278363472316
Epoch (UTC): | 31 March 2023 12:48:43 |
Eccentricity: | 0.0054994 |
inclination: | 97.6685° |
perigee height: | 602 km |
apogee height: | 680 km |
right ascension of ascending node: | 268.4523° |
argument of perigee: | 309.0794° |
revolutions per day: | 14.76278363 |
mean anomaly at epoch: | 50.5531° |
orbit number at epoch: | 47231 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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