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 63920U 26145.61137615 +.00000000 +00000-0 +60030-4 0 00004
2 63920 85.9970 197.3274 0002470 100.9147 259.2314 14.12443426 05
| Epoch (UTC): | 25 May 2026 14:40:22 |
| Eccentricity: | 0.0002470 |
| inclination: | 85.9970° |
| perigee height: | 849 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 197.3274° |
| argument of perigee: | 100.9147° |
| revolutions per day: | 14.12443426 |
| mean anomaly at epoch: | 259.2314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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