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 26022.90595328 +.00000000 +00000-0 +34098-4 0 00008
2 23405 70.9831 88.8120 0004842 252.8139 107.2454 14.15558751 04
| Epoch (UTC): | 22 January 2026 21:44:34 |
| Eccentricity: | 0.0004842 |
| inclination: | 70.9831° |
| perigee height: | 837 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 88.8120° |
| argument of perigee: | 252.8139° |
| revolutions per day: | 14.15558751 |
| mean anomaly at epoch: | 107.2454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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