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 20625U 26039.07733022 +.00000000 +00000-0 +10996-3 0 00000
2 20625 71.0002 0.1018 0014658 340.8198 19.2371 14.15005831 05
| Epoch (UTC): | 08 February 2026 01:51:21 |
| Eccentricity: | 0.0014658 |
| inclination: | 71.0002° |
| perigee height: | 832 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 0.1018° |
| argument of perigee: | 340.8198° |
| revolutions per day: | 14.15005831 |
| mean anomaly at epoch: | 19.2371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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