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 23084.09089788 .00003983 00000-0 74624-3 0 9999
2 28895 98.1388 216.8811 0015718 340.9374 19.1239 14.65280576928727
| Epoch (UTC): | 25 March 2023 02:10:53 |
| Eccentricity: | 0.0015718 |
| inclination: | 98.1388° |
| perigee height: | 665 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 216.8811° |
| argument of perigee: | 340.9374° |
| revolutions per day: | 14.65280576 |
| mean anomaly at epoch: | 19.1239° |
| orbit number at epoch: | 92872 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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