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 63944U 26145.21664949 +.00000000 +00000-0 +14893-3 0 00006
2 63944 70.0009 81.5780 0003061 264.5128 95.5682 14.98338627 07
| Epoch (UTC): | 25 May 2026 05:11:58 |
| Eccentricity: | 0.0003061 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.5780° |
| argument of perigee: | 264.5128° |
| revolutions per day: | 14.98338627 |
| mean anomaly at epoch: | 95.5682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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