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 26129.29700920 +.00000000 +00000-0 +87748-4 0 00003
2 23404 71.0157 332.1778 0017613 257.1598 102.7556 14.13939662 02
| Epoch (UTC): | 09 May 2026 07:07:41 |
| Eccentricity: | 0.0017613 |
| inclination: | 71.0157° |
| perigee height: | 833 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 332.1778° |
| argument of perigee: | 257.1598° |
| revolutions per day: | 14.13939662 |
| mean anomaly at epoch: | 102.7556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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