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 26051.53899110 +.00000000 +00000-0 +54075-4 0 00005
2 31698 97.4464 60.9055 0001831 81.8433 278.3009 15.19148792 04
| Epoch (UTC): | 20 February 2026 12:56:08 |
| Eccentricity: | 0.0001831 |
| inclination: | 97.4464° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 60.9055° |
| argument of perigee: | 81.8433° |
| revolutions per day: | 15.19148792 |
| mean anomaly at epoch: | 278.3009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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