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 23105U 26150.52242969 +.00000000 +00000-0 +32061-3 0 00002
2 23105 81.9380 191.8950 0081075 318.0262 41.4758 14.90634300 07
| Epoch (UTC): | 30 May 2026 12:32:17 |
| Eccentricity: | 0.0081075 |
| inclination: | 81.9380° |
| perigee height: | 539 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 191.8950° |
| argument of perigee: | 318.0262° |
| revolutions per day: | 14.90634300 |
| mean anomaly at epoch: | 41.4758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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