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 43208U 26144.10473947 +.00000000 +00000-0 +00000-0 0 00002
2 43208 56.6307 63.9459 0009456 336.3998 23.5513 1.86230995 09
| Epoch (UTC): | 24 May 2026 02:30:49 |
| Eccentricity: | 0.0009456 |
| inclination: | 56.6307° |
| perigee height: | 21502 km |
| apogee height: | 21554 km |
| right ascension of ascending node: | 63.9459° |
| argument of perigee: | 336.3998° |
| revolutions per day: | 1.86230995 |
| mean anomaly at epoch: | 23.5513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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