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 26155.03481461 +.00003315 00000-0 +87923-4 0 09
2 43477 88.9923 199.7634 0012715 149.5849 294.4457 15.38174758447785
| Epoch (UTC): | 04 June 2026 00:50:07 |
| Eccentricity: | 0.0012715 |
| inclination: | 88.9923° |
| perigee height: | 443 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 199.7634° |
| argument of perigee: | 149.5849° |
| revolutions per day: | 15.38174758 |
| mean anomaly at epoch: | 294.4457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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