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 23029.31756583 .00001785 00000-0 34208-3 0 9999
2 28895 98.1314 162.6929 0016986 147.0802 213.1462 14.64922029920703
| Epoch (UTC): | 29 January 2023 07:37:17 |
| Eccentricity: | 0.0016986 |
| inclination: | 98.1314° |
| perigee height: | 665 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 162.6929° |
| argument of perigee: | 147.0802° |
| revolutions per day: | 14.64922029 |
| mean anomaly at epoch: | 213.1462° |
| orbit number at epoch: | 92070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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