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 31698U 07026A 24281.47912444 .00009678 00000-0 46349-3 0 9993
2 31698 97.4471 287.0434 0002012 83.7020 276.4444 15.19147541960109
| Epoch (UTC): | 07 October 2024 11:29:56 |
| Eccentricity: | 0.0002012 |
| inclination: | 97.4471° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 287.0434° |
| argument of perigee: | 83.7020° |
| revolutions per day: | 15.19147541 |
| mean anomaly at epoch: | 276.4444° |
| orbit number at epoch: | 96010 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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