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 26052.08412014 +.00004968 00000-0 +13593-3 0 04
2 43477 88.9878 213.9035 0010807 189.5462 247.2201 15.37237197431965
| Epoch (UTC): | 21 February 2026 02:01:07 |
| Eccentricity: | 0.0010807 |
| inclination: | 88.9878° |
| perigee height: | 447 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 213.9035° |
| argument of perigee: | 189.5462° |
| revolutions per day: | 15.37237197 |
| mean anomaly at epoch: | 247.2201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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