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 26067.11124971 +.00000000 +00000-0 -74546-5 0 00005
2 23404 71.0137 102.4486 0016394 340.6224 19.4273 14.13933188 00
| Epoch (UTC): | 08 March 2026 02:40:11 |
| Eccentricity: | 0.0016394 |
| inclination: | 71.0137° |
| perigee height: | 834 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 102.4486° |
| argument of perigee: | 340.6224° |
| revolutions per day: | 14.13933188 |
| mean anomaly at epoch: | 19.4273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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