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 31133U 26150.39051213 +.00000000 +00000-0 +33366-3 0 00006
2 31133 98.4359 134.8981 0071800 20.1396 340.2614 14.66647169 02
| Epoch (UTC): | 30 May 2026 09:22:20 |
| Eccentricity: | 0.0071800 |
| inclination: | 98.4359° |
| perigee height: | 621 km |
| apogee height: | 722 km |
| right ascension of ascending node: | 134.8981° |
| argument of perigee: | 20.1396° |
| revolutions per day: | 14.66647169 |
| mean anomaly at epoch: | 340.2614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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