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 17129U 86019Y 22222.35733715 .00000066 00000-0 45854-4 0 9990
2 17129 98.4587 275.7492 0032964 358.9806 129.6205 14.25047658806205
| Epoch (UTC): | 10 August 2022 08:34:33 |
| Eccentricity: | 0.0032964 |
| inclination: | 98.4587° |
| perigee height: | 784 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 275.7492° |
| argument of perigee: | 358.9806° |
| revolutions per day: | 14.25047658 |
| mean anomaly at epoch: | 129.6205° |
| orbit number at epoch: | 80620 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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