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 43476U 18047A 26069.53342573 +.00006019 00000-0 +16335-3 0 09
2 43476 88.9902 211.4981 0013478 129.3167 332.5817 15.37453982434647
| Epoch (UTC): | 10 March 2026 12:48:07 |
| Eccentricity: | 0.0013478 |
| inclination: | 88.9902° |
| perigee height: | 444 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 211.4981° |
| argument of perigee: | 129.3167° |
| revolutions per day: | 15.37453982 |
| mean anomaly at epoch: | 332.5817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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