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 25397U 98043D 23086.84665100 .00000263 00000-0 13451-3 0 9997
2 25397 98.8597 43.6429 0001874 44.5317 315.6012 14.23846517283750
Epoch (UTC): | 27 March 2023 20:19:10 |
Eccentricity: | 0.0001874 |
inclination: | 98.8597° |
perigee height: | 811 km |
apogee height: | 814 km |
right ascension of ascending node: | 43.6429° |
argument of perigee: | 44.5317° |
revolutions per day: | 14.23846517 |
mean anomaly at epoch: | 315.6012° |
orbit number at epoch: | 28375 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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