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 26104.20159067 +.00000000 +00000-0 +11367-3 0 00008
2 31133 98.4342 87.4088 0071732 162.6853 197.6821 14.66542708 06
| Epoch (UTC): | 14 April 2026 04:50:17 |
| Eccentricity: | 0.0071732 |
| inclination: | 98.4342° |
| perigee height: | 622 km |
| apogee height: | 723 km |
| right ascension of ascending node: | 87.4088° |
| argument of perigee: | 162.6853° |
| revolutions per day: | 14.66542708 |
| mean anomaly at epoch: | 197.6821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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