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 23156.10078870 .00000211 00000-0 73686-4 0 9992
2 16864 74.0303 21.9857 0033480 303.9195 55.8778 14.40993746936436
| Epoch (UTC): | 05 June 2023 02:25:08 |
| Eccentricity: | 0.0033480 |
| inclination: | 74.0303° |
| perigee height: | 731 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 21.9857° |
| argument of perigee: | 303.9195° |
| revolutions per day: | 14.40993746 |
| mean anomaly at epoch: | 55.8778° |
| orbit number at epoch: | 93643 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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