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 15388U 84114C 22220.73620535 .00000358 00000-0 45463-3 0 9993
2 15388 7.2368 86.0681 6917184 284.7218 12.8142 2.68334168266766
| Epoch (UTC): | 08 August 2022 17:40:08 |
| Eccentricity: | 0.6917184 |
| inclination: | 7.2368° |
| perigee height: | 365 km |
| apogee height: | 30628 km |
| right ascension of ascending node: | 86.0681° |
| argument of perigee: | 284.7218° |
| revolutions per day: | 2.68334168 |
| mean anomaly at epoch: | 12.8142° |
| orbit number at epoch: | 26676 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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