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 23705U 26020.93196171 +.00000000 +00000-0 -56341-4 0 00001
2 23705 71.0217 280.5223 0013358 202.8662 157.1867 14.15489526 05
| Epoch (UTC): | 20 January 2026 22:22:01 |
| Eccentricity: | 0.0013358 |
| inclination: | 71.0217° |
| perigee height: | 831 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 280.5223° |
| argument of perigee: | 202.8662° |
| revolutions per day: | 14.15489526 |
| mean anomaly at epoch: | 157.1867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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