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 26088.16832476 +.00000000 +00000-0 +14008-3 0 00001
2 23466 82.9253 46.1044 0033165 264.7167 106.5238 13.74724211 09
| Epoch (UTC): | 29 March 2026 04:02:23 |
| Eccentricity: | 0.0033165 |
| inclination: | 82.9253° |
| perigee height: | 958 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 46.1044° |
| argument of perigee: | 264.7167° |
| revolutions per day: | 13.74724211 |
| mean anomaly at epoch: | 106.5238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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