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 23051U 26149.59674713 +.00000000 +00000-0 +00000-0 0 00008
2 23051 14.4137 13.8198 0006225 45.3822 146.5450 0.98904102 00
| Epoch (UTC): | 29 May 2026 14:19:18 |
| Eccentricity: | 0.0006225 |
| inclination: | 14.4137° |
| perigee height: | 36148 km |
| apogee height: | 36201 km |
| right ascension of ascending node: | 13.8198° |
| argument of perigee: | 45.3822° |
| revolutions per day: | 0.98904102 |
| mean anomaly at epoch: | 146.5450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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