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 28376U 04026A 23336.89910911 .00002273 00000-0 50447-3 0 9990
2 28376 98.2296 278.4645 0001361 61.9884 298.1452 14.58029499 30923
Epoch (UTC): | 02 December 2023 21:34:43 |
Eccentricity: | 0.0001361 |
inclination: | 98.2296° |
perigee height: | 698 km |
apogee height: | 700 km |
right ascension of ascending node: | 278.4645° |
argument of perigee: | 61.9884° |
revolutions per day: | 14.58029499 |
mean anomaly at epoch: | 298.1452° |
orbit number at epoch: | 3092 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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