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 63894U 26145.26406654 +.00000000 +00000-0 +77906-3 0 00006
2 63894 43.0025 103.3550 0001519 261.5753 98.4926 15.27599592 00
| Epoch (UTC): | 25 May 2026 06:20:15 |
| Eccentricity: | 0.0001519 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.3550° |
| argument of perigee: | 261.5753° |
| revolutions per day: | 15.27599592 |
| mean anomaly at epoch: | 98.4926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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