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 31114U 07010B 23152.40124099 .00000160 00000-0 92999-4 0 9999
2 31114 98.2784 307.0375 0059539 1.7620 358.3756 14.19572935836068
| Epoch (UTC): | 01 June 2023 09:37:47 |
| Eccentricity: | 0.0059539 |
| inclination: | 98.2784° |
| perigee height: | 784 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 307.0375° |
| argument of perigee: | 1.7620° |
| revolutions per day: | 14.19572935 |
| mean anomaly at epoch: | 358.3756° |
| orbit number at epoch: | 83606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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