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 31306U 26145.14824964 +.00000000 +00000-0 +00000-0 0 00002
2 31306 1.2646 81.7455 0005102 350.4596 199.3973 1.00272980 04
| Epoch (UTC): | 25 May 2026 03:33:28 |
| Eccentricity: | 0.0005102 |
| inclination: | 1.2646° |
| perigee height: | 35765 km |
| apogee height: | 35808 km |
| right ascension of ascending node: | 81.7455° |
| argument of perigee: | 350.4596° |
| revolutions per day: | 1.00272980 |
| mean anomaly at epoch: | 199.3973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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