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 23405U 26041.42007877 +.00000000 +00000-0 +13606-3 0 00004
2 23405 70.9817 49.8586 0004218 234.2768 125.7963 14.15557981 04
| Epoch (UTC): | 10 February 2026 10:04:54 |
| Eccentricity: | 0.0004218 |
| inclination: | 70.9817° |
| perigee height: | 837 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 49.8586° |
| argument of perigee: | 234.2768° |
| revolutions per day: | 14.15557981 |
| mean anomaly at epoch: | 125.7963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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