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 61910U 26145.60675947 +.00000000 +00000-0 +00000-0 0 00002
2 61910 0.0477 113.2431 0000868 293.3863 171.0140 1.00272038 05
| Epoch (UTC): | 25 May 2026 14:33:44 |
| Eccentricity: | 0.0000868 |
| inclination: | 0.0477° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 113.2431° |
| argument of perigee: | 293.3863° |
| revolutions per day: | 1.00272038 |
| mean anomaly at epoch: | 171.0140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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