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 43057U 26143.89110030 +.00000000 +00000-0 +00000-0 0 00000
2 43057 55.0789 222.1733 0003554 287.2747 72.7400 1.70474769 04
| Epoch (UTC): | 23 May 2026 21:23:11 |
| Eccentricity: | 0.0003554 |
| inclination: | 55.0789° |
| perigee height: | 23212 km |
| apogee height: | 23233 km |
| right ascension of ascending node: | 222.1733° |
| argument of perigee: | 287.2747° |
| revolutions per day: | 1.70474769 |
| mean anomaly at epoch: | 72.7400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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