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 16864U 86052B 23150.13027828 .00000211 00000-0 73404-4 0 9994
2 16864 74.0309 33.0401 0033362 316.0836 43.7668 14.40990677935575
| Epoch (UTC): | 30 May 2023 03:07:36 |
| Eccentricity: | 0.0033362 |
| inclination: | 74.0309° |
| perigee height: | 731 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 33.0401° |
| argument of perigee: | 316.0836° |
| revolutions per day: | 14.40990677 |
| mean anomaly at epoch: | 43.7668° |
| orbit number at epoch: | 93557 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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