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 23464U 26054.20469362 +.00000000 +00000-0 +79026-4 0 00009
2 23464 82.9248 102.9946 0042447 105.4174 255.1676 13.73060992 00
| Epoch (UTC): | 23 February 2026 04:54:45 |
| Eccentricity: | 0.0042447 |
| inclination: | 82.9248° |
| perigee height: | 957 km |
| apogee height: | 1020 km |
| right ascension of ascending node: | 102.9946° |
| argument of perigee: | 105.4174° |
| revolutions per day: | 13.73060992 |
| mean anomaly at epoch: | 255.1676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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