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 43207U 26144.03828042 +.00000000 +00000-0 +00000-0 0 00003
2 43207 56.6312 63.9440 0007967 11.9545 348.0589 1.86231141 05
| Epoch (UTC): | 24 May 2026 00:55:07 |
| Eccentricity: | 0.0007967 |
| inclination: | 56.6312° |
| perigee height: | 21506 km |
| apogee height: | 21550 km |
| right ascension of ascending node: | 63.9440° |
| argument of perigee: | 11.9545° |
| revolutions per day: | 1.86231141 |
| mean anomaly at epoch: | 348.0589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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