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 61631U 26145.24589500 +.00000000 +00000-0 +27717-4 0 00009
2 61631 43.0027 85.7087 0001093 258.1789 101.8940 15.27579476 09
| Epoch (UTC): | 25 May 2026 05:54:05 |
| Eccentricity: | 0.0001093 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 85.7087° |
| argument of perigee: | 258.1789° |
| revolutions per day: | 15.27579476 |
| mean anomaly at epoch: | 101.8940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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