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 23465U 26104.15069432 +.00000000 +00000-0 +13161-4 0 00002
2 23465 82.9254 70.5089 0037193 347.9375 21.7033 13.72022246 07
| Epoch (UTC): | 14 April 2026 03:36:59 |
| Eccentricity: | 0.0037193 |
| inclination: | 82.9254° |
| perigee height: | 965 km |
| apogee height: | 1020 km |
| right ascension of ascending node: | 70.5089° |
| argument of perigee: | 347.9375° |
| revolutions per day: | 13.72022246 |
| mean anomaly at epoch: | 21.7033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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