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 16682U 86030B 23157.08408396 .00000112 00000-0 47292-4 0 9998
2 16682 74.0240 182.4089 0014979 346.5470 30.3482 14.36276648944074
| Epoch (UTC): | 06 June 2023 02:01:04 |
| Eccentricity: | 0.0014979 |
| inclination: | 74.0240° |
| perigee height: | 760 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 182.4089° |
| argument of perigee: | 346.5470° |
| revolutions per day: | 14.36276648 |
| mean anomaly at epoch: | 30.3482° |
| orbit number at epoch: | 94407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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