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 11416U 79057A 23150.49333979 .00000317 00000-0 12955-3 0 9995
2 11416 98.6516 166.7715 0009412 319.7778 40.2709 14.34054988291258
| Epoch (UTC): | 30 May 2023 11:50:24 |
| Eccentricity: | 0.0009412 |
| inclination: | 98.6516° |
| perigee height: | 771 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 166.7715° |
| argument of perigee: | 319.7778° |
| revolutions per day: | 14.34054988 |
| mean anomaly at epoch: | 40.2709° |
| orbit number at epoch: | 29125 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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