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 28895U 05043F 23335.28974975 .00003921 00000-0 71541-3 0 9997
2 28895 98.1760 106.3890 0015011 265.1720 94.7770 14.66489019965522
Epoch (UTC): | 01 December 2023 06:57:14 |
Eccentricity: | 0.0015011 |
inclination: | 98.1760° |
perigee height: | 662 km |
apogee height: | 683 km |
right ascension of ascending node: | 106.3890° |
argument of perigee: | 265.1720° |
revolutions per day: | 14.66489019 |
mean anomaly at epoch: | 94.7770° |
orbit number at epoch: | 96552 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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