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 23150.68858366 .00001580 00000-0 78387-4 0 9994
2 31698 97.4448 158.3214 0001724 86.1378 274.0054 15.19153772884177
| Epoch (UTC): | 30 May 2023 16:31:33 |
| Eccentricity: | 0.0001724 |
| inclination: | 97.4448° |
| perigee height: | 507 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 158.3214° |
| argument of perigee: | 86.1378° |
| revolutions per day: | 15.19153772 |
| mean anomaly at epoch: | 274.0054° |
| orbit number at epoch: | 88417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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