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 31490U 26145.54782623 +.00000000 +00000-0 +87878-4 0 00007
2 31490 98.2674 5.3924 0020335 350.7988 9.2849 14.82635399 03
| Epoch (UTC): | 25 May 2026 13:08:52 |
| Eccentricity: | 0.0020335 |
| inclination: | 98.2674° |
| perigee height: | 607 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 5.3924° |
| argument of perigee: | 350.7988° |
| revolutions per day: | 14.82635399 |
| mean anomaly at epoch: | 9.2849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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