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 63929U 26145.54627530 +.00000000 +00000-0 +15930-3 0 00003
2 63929 70.0008 80.7227 0003330 266.2853 93.7925 14.98326735 06
| Epoch (UTC): | 25 May 2026 13:06:38 |
| Eccentricity: | 0.0003330 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.7227° |
| argument of perigee: | 266.2853° |
| revolutions per day: | 14.98326735 |
| mean anomaly at epoch: | 93.7925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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