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 27825U 26145.23601895 +.00000000 +00000-0 +00000-0 0 00009
2 27825 8.8065 32.0735 0003289 359.1067 340.6192 1.00273320 09
| Epoch (UTC): | 25 May 2026 05:39:52 |
| Eccentricity: | 0.0003289 |
| inclination: | 8.8065° |
| perigee height: | 35772 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 32.0735° |
| argument of perigee: | 359.1067° |
| revolutions per day: | 1.00273320 |
| mean anomaly at epoch: | 340.6192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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