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 23404U 26156.60478375 +.00000000 +00000-0 -65252-4 0 00001
2 23404 71.0142 274.9702 0016972 219.6712 140.3170 14.13936653 01
| Epoch (UTC): | 05 June 2026 14:30:53 |
| Eccentricity: | 0.0016972 |
| inclination: | 71.0142° |
| perigee height: | 834 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 274.9702° |
| argument of perigee: | 219.6712° |
| revolutions per day: | 14.13936653 |
| mean anomaly at epoch: | 140.3170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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