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 25112.42518019 .00002526 00000-0 12342-3 0 9993
2 31698 97.4447 121.1422 0001728 84.2063 275.9368 15.19156226989349
| Epoch (UTC): | 22 April 2025 10:12:15 |
| Eccentricity: | 0.0001728 |
| inclination: | 97.4447° |
| perigee height: | 507 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 121.1422° |
| argument of perigee: | 84.2063° |
| revolutions per day: | 15.19156226 |
| mean anomaly at epoch: | 275.9368° |
| orbit number at epoch: | 98934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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