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 28419U 04037A 23088.47433589 .00000055 00000-0 31212-3 0 9994
2 28419 82.4898 342.3596 0015899 329.4957 30.5200 12.45638205841692
Epoch (UTC): | 29 March 2023 11:23:02 |
Eccentricity: | 0.0015899 |
inclination: | 82.4898° |
perigee height: | 1470 km |
apogee height: | 1495 km |
right ascension of ascending node: | 342.3596° |
argument of perigee: | 329.4957° |
revolutions per day: | 12.45638205 |
mean anomaly at epoch: | 30.5200° |
orbit number at epoch: | 84169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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