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 23150.07470671 .00000318 00000-0 12991-3 0 9991
2 11416 98.6516 166.3525 0009434 321.1266 38.9239 14.34054670291403
| Epoch (UTC): | 30 May 2023 01:47:34 |
| Eccentricity: | 0.0009434 |
| inclination: | 98.6516° |
| perigee height: | 771 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 166.3525° |
| argument of perigee: | 321.1266° |
| revolutions per day: | 14.34054670 |
| mean anomaly at epoch: | 38.9239° |
| orbit number at epoch: | 29140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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