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 26017.79901086 +.00000000 +00000-0 +84352-6 0 00002
2 20625 70.9995 44.7920 0013598 11.6107 348.5327 14.15007902 05
| Epoch (UTC): | 17 January 2026 19:10:34 |
| Eccentricity: | 0.0013598 |
| inclination: | 70.9995° |
| perigee height: | 832 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 44.7920° |
| argument of perigee: | 11.6107° |
| revolutions per day: | 14.15007902 |
| mean anomaly at epoch: | 348.5327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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