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 31128U 26150.85169845 +.00000000 +00000-0 +26098-3 0 00006
2 31128 98.4379 120.3955 0085840 133.9075 226.9256 14.63725703 05
| Epoch (UTC): | 30 May 2026 20:26:26 |
| Eccentricity: | 0.0085840 |
| inclination: | 98.4379° |
| perigee height: | 621 km |
| apogee height: | 742 km |
| right ascension of ascending node: | 120.3955° |
| argument of perigee: | 133.9075° |
| revolutions per day: | 14.63725703 |
| mean anomaly at epoch: | 226.9256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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