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 08860U 76047A 23088.42588375 .00000200 00000-0 28998-3 0 9990
2 08860 99.9095 252.9998 0042709 104.4812 285.3683 13.67809474335624
| Epoch (UTC): | 29 March 2023 10:13:16 |
| Eccentricity: | 0.0042709 |
| inclination: | 99.9095° |
| perigee height: | 976 km |
| apogee height: | 1039 km |
| right ascension of ascending node: | 252.9998° |
| argument of perigee: | 104.4812° |
| revolutions per day: | 13.67809474 |
| mean anomaly at epoch: | 285.3683° |
| orbit number at epoch: | 33562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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