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 28650U 05017B 23334.50525621 .00008155 00000-0 74595-3 0 9997
2 28650 97.9691 312.0850 0018696 262.8367 97.0727 14.95127310 7199
| Epoch (UTC): | 30 November 2023 12:07:34 |
| Eccentricity: | 0.0018696 |
| inclination: | 97.9691° |
| perigee height: | 569 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 312.0850° |
| argument of perigee: | 262.8367° |
| revolutions per day: | 14.95127310 |
| mean anomaly at epoch: | 97.0727° |
| orbit number at epoch: | 719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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