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 26102.52105116 +.00000000 +00000-0 +26748-4 0 00003
2 31698 97.4462 111.1648 0002009 87.6779 272.4685 15.19152757 05
| Epoch (UTC): | 12 April 2026 12:30:18 |
| Eccentricity: | 0.0002009 |
| inclination: | 97.4462° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 111.1648° |
| argument of perigee: | 87.6779° |
| revolutions per day: | 15.19152757 |
| mean anomaly at epoch: | 272.4685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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