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 31130U 26150.88862972 +.00000000 +00000-0 +28573-3 0 00003
2 31130 98.4451 124.9221 0084613 124.6280 236.2937 14.64824000 08
| Epoch (UTC): | 30 May 2026 21:19:37 |
| Eccentricity: | 0.0084613 |
| inclination: | 98.4451° |
| perigee height: | 618 km |
| apogee height: | 737 km |
| right ascension of ascending node: | 124.9221° |
| argument of perigee: | 124.6280° |
| revolutions per day: | 14.64824000 |
| mean anomaly at epoch: | 236.2937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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