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 43803U 26101.43249684 +.00000000 +00000-0 +42826-3 0 00006
2 43803 97.4190 164.1254 0007148 140.5208 219.6556 15.31603261 05
| Epoch (UTC): | 11 April 2026 10:22:47 |
| Eccentricity: | 0.0007148 |
| inclination: | 97.4190° |
| perigee height: | 466 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 164.1254° |
| argument of perigee: | 140.5208° |
| revolutions per day: | 15.31603261 |
| mean anomaly at epoch: | 219.6556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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