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 23155.86060154 .00000136 00000-0 55677-4 0 9990
2 16682 74.0242 184.6573 0014934 349.0190 184.2857 14.36276306943587
| Epoch (UTC): | 04 June 2023 20:39:15 |
| Eccentricity: | 0.0014934 |
| inclination: | 74.0242° |
| perigee height: | 760 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 184.6573° |
| argument of perigee: | 349.0190° |
| revolutions per day: | 14.36276306 |
| mean anomaly at epoch: | 184.2857° |
| orbit number at epoch: | 94358 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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