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 23342.55609562 .00000188 00000-0 96768-4 0 9993
2 17129 98.3885 21.5975 0033129 17.4405 107.6801 14.25335129875605
| Epoch (UTC): | 08 December 2023 13:20:46 |
| Eccentricity: | 0.0033129 |
| inclination: | 98.3885° |
| perigee height: | 783 km |
| apogee height: | 831 km |
| right ascension of ascending node: | 21.5975° |
| argument of perigee: | 17.4405° |
| revolutions per day: | 14.25335129 |
| mean anomaly at epoch: | 107.6801° |
| orbit number at epoch: | 87560 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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