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 26107.08032398 +.00002219 00000-0 +59555-4 0 03
2 43476 88.9954 206.3412 0010040 5.3398 73.3899 15.37835136440414
| Epoch (UTC): | 17 April 2026 01:55:39 |
| Eccentricity: | 0.0010040 |
| inclination: | 88.9954° |
| perigee height: | 445 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 206.3412° |
| argument of perigee: | 5.3398° |
| revolutions per day: | 15.37835136 |
| mean anomaly at epoch: | 73.3899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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