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 63891U 26145.25652406 +.00000000 +00000-0 +58050-3 0 00009
2 63891 43.0012 104.1662 0001707 233.0582 127.0114 15.27587127 08
| Epoch (UTC): | 25 May 2026 06:09:23 |
| Eccentricity: | 0.0001707 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.1662° |
| argument of perigee: | 233.0582° |
| revolutions per day: | 15.27587127 |
| mean anomaly at epoch: | 127.0114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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