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 05485U 26088.07879288 +.00000000 +00000-0 -11946-5 0 00005
2 05485 32.0566 89.7517 0639903 229.3951 124.9243 12.74248425 08
| Epoch (UTC): | 29 March 2026 01:53:27 |
| Eccentricity: | 0.0639903 |
| inclination: | 32.0566° |
| perigee height: | 869 km |
| apogee height: | 1860 km |
| right ascension of ascending node: | 89.7517° |
| argument of perigee: | 229.3951° |
| revolutions per day: | 12.74248425 |
| mean anomaly at epoch: | 124.9243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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