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 23147.14501931 .00000253 00000-0 86374-4 0 9999
2 16864 74.0310 38.5670 0033271 322.2111 37.6708 14.40989141935402
| Epoch (UTC): | 27 May 2023 03:28:49 |
| Eccentricity: | 0.0033271 |
| inclination: | 74.0310° |
| perigee height: | 731 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 38.5670° |
| argument of perigee: | 322.2111° |
| revolutions per day: | 14.40989141 |
| mean anomaly at epoch: | 37.6708° |
| orbit number at epoch: | 93540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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