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 03955U 69046E 25220.60555884 .00000590 00000-0 00000-0 0 9993
2 03955 62.5463 63.7142 8192423 138.0677 0.4662 0.21421919 6344
| Epoch (UTC): | 08 August 2025 14:32:00 |
| Eccentricity: | 0.8192423 |
| inclination: | 62.5463° |
| perigee height: | 14948 km |
| apogee height: | 208264 km |
| right ascension of ascending node: | 63.7142° |
| argument of perigee: | 138.0677° |
| revolutions per day: | 0.21421919 |
| mean anomaly at epoch: | 0.4662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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