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 22027.15535326 -.00000738 00000-0 -31974-4 0 9993
2 31698 97.4458 36.7655 0001685 69.3777 355.0667 15.19145717810672
| Epoch (UTC): | 27 January 2022 03:43:42 |
| Eccentricity: | 0.0001685 |
| inclination: | 97.4458° |
| perigee height: | 507 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 36.7655° |
| argument of perigee: | 69.3777° |
| revolutions per day: | 15.19145717 |
| mean anomaly at epoch: | 355.0667° |
| orbit number at epoch: | 81067 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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