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 23339.31532562 .00002247 00000-0 41354-3 0 9996
2 28895 98.1753 110.3994 0015042 251.5002 108.4567 14.66515655965882
Epoch (UTC): | 05 December 2023 07:34:04 |
Eccentricity: | 0.0015042 |
inclination: | 98.1753° |
perigee height: | 661 km |
apogee height: | 683 km |
right ascension of ascending node: | 110.3994° |
argument of perigee: | 251.5002° |
revolutions per day: | 14.66515655 |
mean anomaly at epoch: | 108.4567° |
orbit number at epoch: | 96588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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