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 26069.94107961 +.00000000 +00000-0 -45109-4 0 00000
2 23404 71.0134 96.5202 0016624 336.3234 23.7122 14.13932841 01
| Epoch (UTC): | 10 March 2026 22:35:09 |
| Eccentricity: | 0.0016624 |
| inclination: | 71.0134° |
| perigee height: | 834 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 96.5202° |
| argument of perigee: | 336.3234° |
| revolutions per day: | 14.13932841 |
| mean anomaly at epoch: | 23.7122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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