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 61918U 26145.49547237 +.00000000 +00000-0 +49843-3 0 00008
2 61918 43.0020 211.8644 0001246 275.3733 84.6977 15.27582842 00
| Epoch (UTC): | 25 May 2026 11:53:28 |
| Eccentricity: | 0.0001246 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.8644° |
| argument of perigee: | 275.3733° |
| revolutions per day: | 15.27582842 |
| mean anomaly at epoch: | 84.6977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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