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 63849U 26145.28456972 +.00000000 +00000-0 +85364-3 0 00003
2 63849 42.9970 2.1070 0000858 290.9065 69.1695 15.27578238 09
| Epoch (UTC): | 25 May 2026 06:49:46 |
| Eccentricity: | 0.0000858 |
| inclination: | 42.9970° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 2.1070° |
| argument of perigee: | 290.9065° |
| revolutions per day: | 15.27578238 |
| mean anomaly at epoch: | 69.1695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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