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 11963U 80073B 22222.13589687 .00000165 00000-0 84431-4 0 9991
2 11963 81.2762 102.1159 0076136 155.2705 205.2148 14.09772095155136
| Epoch (UTC): | 10 August 2022 03:15:41 |
| Eccentricity: | 0.0076136 |
| inclination: | 81.2762° |
| perigee height: | 805 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 102.1159° |
| argument of perigee: | 155.2705° |
| revolutions per day: | 14.09772095 |
| mean anomaly at epoch: | 205.2148° |
| orbit number at epoch: | 15513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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