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 23079.58390521 .00002492 00000-0 47071-3 0 9997
2 28895 98.1380 212.4194 0015981 355.4364 4.6691 14.65248119927836
| Epoch (UTC): | 20 March 2023 14:00:49 |
| Eccentricity: | 0.0015981 |
| inclination: | 98.1380° |
| perigee height: | 665 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 212.4194° |
| argument of perigee: | 355.4364° |
| revolutions per day: | 14.65248119 |
| mean anomaly at epoch: | 4.6691° |
| orbit number at epoch: | 92783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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