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 63898U 26145.19482707 +.00000000 +00000-0 +10161-2 0 00004
2 63898 43.0016 103.6953 0001310 278.1059 81.9644 15.27589686 03
| Epoch (UTC): | 25 May 2026 04:40:33 |
| Eccentricity: | 0.0001310 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.6953° |
| argument of perigee: | 278.1059° |
| revolutions per day: | 15.27589686 |
| mean anomaly at epoch: | 81.9644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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