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 28891U 05043B 23088.81374749 .00001016 00000-0 21171-3 0 9997
2 28891 98.1536 213.3655 0016441 8.9807 351.1657 14.62011074928772
| Epoch (UTC): | 29 March 2023 19:31:47 |
| Eccentricity: | 0.0016441 |
| inclination: | 98.1536° |
| perigee height: | 675 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 213.3655° |
| argument of perigee: | 8.9807° |
| revolutions per day: | 14.62011074 |
| mean anomaly at epoch: | 351.1657° |
| orbit number at epoch: | 92877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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