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 23180U 26088.07603336 +.00000000 +00000-0 +15866-3 0 00008
2 23180 82.9442 64.3338 0027613 229.8318 200.8042 13.78294087 09
| Epoch (UTC): | 29 March 2026 01:49:29 |
| Eccentricity: | 0.0027613 |
| inclination: | 82.9442° |
| perigee height: | 950 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 64.3338° |
| argument of perigee: | 229.8318° |
| revolutions per day: | 13.78294087 |
| mean anomaly at epoch: | 200.8042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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