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 43477U 18047B 26053.12578679 +.00005301 00000-0 +14498-3 0 07
2 43477 88.9878 213.7599 0011015 185.6436 251.7160 15.37247840432127
| Epoch (UTC): | 22 February 2026 03:01:07 |
| Eccentricity: | 0.0011015 |
| inclination: | 88.9878° |
| perigee height: | 447 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 213.7599° |
| argument of perigee: | 185.6436° |
| revolutions per day: | 15.37247840 |
| mean anomaly at epoch: | 251.7160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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