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 23028.65993347 -.00000722 00000-0 -31200-4 0 9996
2 31698 97.4459 38.0305 0002280 100.5167 37.7518 15.19144402866303
| Epoch (UTC): | 28 January 2023 15:50:18 |
| Eccentricity: | 0.0002280 |
| inclination: | 97.4459° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 38.0305° |
| argument of perigee: | 100.5167° |
| revolutions per day: | 15.19144402 |
| mean anomaly at epoch: | 37.7518° |
| orbit number at epoch: | 86630 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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