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 23089.89521688 .00003700 00000-0 69329-3 0 9995
2 28895 98.1393 222.6286 0015412 321.8594 38.1517 14.65318869929578
| Epoch (UTC): | 30 March 2023 21:29:06 |
| Eccentricity: | 0.0015412 |
| inclination: | 98.1393° |
| perigee height: | 665 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 222.6286° |
| argument of perigee: | 321.8594° |
| revolutions per day: | 14.65318869 |
| mean anomaly at epoch: | 38.1517° |
| orbit number at epoch: | 92957 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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