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 23466U 26128.21988829 +.00000000 +00000-0 +29881-4 0 00002
2 23466 82.9278 16.3827 0035139 151.0026 324.5365 13.74729552 05
| Epoch (UTC): | 08 May 2026 05:16:38 |
| Eccentricity: | 0.0035139 |
| inclination: | 82.9278° |
| perigee height: | 957 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 16.3827° |
| argument of perigee: | 151.0026° |
| revolutions per day: | 13.74729552 |
| mean anomaly at epoch: | 324.5365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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