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 31115U 26150.33683769 +.00000000 +00000-0 +00000-0 0 00003
2 31115 50.9352 219.8720 0001899 320.6375 39.4337 1.77349284 03
| Epoch (UTC): | 30 May 2026 08:05:02 |
| Eccentricity: | 0.0001899 |
| inclination: | 50.9352° |
| perigee height: | 22447 km |
| apogee height: | 22458 km |
| right ascension of ascending node: | 219.8720° |
| argument of perigee: | 320.6375° |
| revolutions per day: | 1.77349284 |
| mean anomaly at epoch: | 39.4337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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