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 28897U 05043H 23272.32786045 .00002779 00000-0 50636-3 0 9995
2 28897 98.1643 44.7643 0016583 94.0833 326.4014 14.66753847948535
| Epoch (UTC): | 29 September 2023 07:52:07 |
| Eccentricity: | 0.0016583 |
| inclination: | 98.1643° |
| perigee height: | 660 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 44.7643° |
| argument of perigee: | 94.0833° |
| revolutions per day: | 14.66753847 |
| mean anomaly at epoch: | 326.4014° |
| orbit number at epoch: | 94853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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