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 23148.34134081 .00001504 00000-0 28534-3 0 9991
2 28895 98.1509 280.5569 0017351 132.3516 227.9160 14.65602381938136
| Epoch (UTC): | 28 May 2023 08:11:31 |
| Eccentricity: | 0.0017351 |
| inclination: | 98.1509° |
| perigee height: | 663 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 280.5569° |
| argument of perigee: | 132.3516° |
| revolutions per day: | 14.65602381 |
| mean anomaly at epoch: | 227.9160° |
| orbit number at epoch: | 93813 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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