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 31125U 26145.39104270 +.00000000 +00000-0 +11688-3 0 00006
2 31125 98.3132 120.3617 0040264 122.9645 237.5442 14.70662480 00
| Epoch (UTC): | 25 May 2026 09:23:06 |
| Eccentricity: | 0.0040264 |
| inclination: | 98.3132° |
| perigee height: | 631 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 120.3617° |
| argument of perigee: | 122.9645° |
| revolutions per day: | 14.70662480 |
| mean anomaly at epoch: | 237.5442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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