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 63974U 26145.25310999 +.00000000 +00000-0 +92852-3 0 00007
2 63974 43.0024 100.5374 0001459 258.5901 101.4787 15.27593753 08
| Epoch (UTC): | 25 May 2026 06:04:28 |
| Eccentricity: | 0.0001459 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.5374° |
| argument of perigee: | 258.5901° |
| revolutions per day: | 15.27593753 |
| mean anomaly at epoch: | 101.4787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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