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 31307U 26145.56691501 +.00000000 +00000-0 +00000-0 0 00008
2 31307 2.9174 80.1753 0004533 1.4257 280.6347 1.00272401 04
| Epoch (UTC): | 25 May 2026 13:36:21 |
| Eccentricity: | 0.0004533 |
| inclination: | 2.9174° |
| perigee height: | 35767 km |
| apogee height: | 35806 km |
| right ascension of ascending node: | 80.1753° |
| argument of perigee: | 1.4257° |
| revolutions per day: | 1.00272401 |
| mean anomaly at epoch: | 280.6347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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