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 63889U 26145.13273008 +.00000000 +00000-0 +26717-3 0 00005
2 63889 70.0023 41.6894 0002665 269.3083 90.7771 14.98337801 05
| Epoch (UTC): | 25 May 2026 03:11:07 |
| Eccentricity: | 0.0002665 |
| inclination: | 70.0023° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.6894° |
| argument of perigee: | 269.3083° |
| revolutions per day: | 14.98337801 |
| mean anomaly at epoch: | 90.7771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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