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 26162.61817294 +.00000000 +00000-0 -25842-4 0 00007
2 23404 71.0135 262.3731 0016665 210.5346 149.4808 14.13935352 01
| Epoch (UTC): | 11 June 2026 14:50:10 |
| Eccentricity: | 0.0016665 |
| inclination: | 71.0135° |
| perigee height: | 834 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 262.3731° |
| argument of perigee: | 210.5346° |
| revolutions per day: | 14.13935352 |
| mean anomaly at epoch: | 149.4808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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