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 31113U 26145.35078503 +.00000000 +00000-0 +48990-4 0 00005
2 31113 98.3486 128.0832 0012206 269.5275 90.4510 14.31020487 09
| Epoch (UTC): | 25 May 2026 08:25:07 |
| Eccentricity: | 0.0012206 |
| inclination: | 98.3486° |
| perigee height: | 780 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 128.0832° |
| argument of perigee: | 269.5275° |
| revolutions per day: | 14.31020487 |
| mean anomaly at epoch: | 90.4510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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