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 26152.44920595 +.00000000 +00000-0 +41227-4 0 00004
2 31698 97.4458 160.3801 0001803 98.4388 261.7051 15.19149262 09
| Epoch (UTC): | 01 June 2026 10:46:51 |
| Eccentricity: | 0.0001803 |
| inclination: | 97.4458° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 160.3801° |
| argument of perigee: | 98.4388° |
| revolutions per day: | 15.19149262 |
| mean anomaly at epoch: | 261.7051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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