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 is defined by the following mean orbital elements,
1 31698U 26150.34141933 +.00000000 +00000-0 +60517-4 0 00005
2 31698 97.4458 158.3023 0001861 101.5968 258.5476 15.19152389 05
| Epoch (UTC): | 30 May 2026 08:11:38 |
| Eccentricity: | 0.0001861 |
| inclination: | 97.4458° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 158.3023° |
| argument of perigee: | 101.5968° |
| revolutions per day: | 15.19152389 |
| mean anomaly at epoch: | 258.5476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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