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 26021.49266307 +.00000000 +00000-0 +61996-4 0 00000
2 23405 70.9832 91.7853 0004842 253.7974 106.2616 14.15558314 02
| Epoch (UTC): | 21 January 2026 11:49:26 |
| Eccentricity: | 0.0004842 |
| inclination: | 70.9832° |
| perigee height: | 837 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 91.7853° |
| argument of perigee: | 253.7974° |
| revolutions per day: | 14.15558314 |
| mean anomaly at epoch: | 106.2616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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