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 63828U 26145.25046315 +.00000000 +00000-0 +56601-3 0 00005
2 63828 43.0008 100.1618 0001124 262.6035 97.4689 15.27617594 03
| Epoch (UTC): | 25 May 2026 06:00:40 |
| Eccentricity: | 0.0001124 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.1618° |
| argument of perigee: | 262.6035° |
| revolutions per day: | 15.27617594 |
| mean anomaly at epoch: | 97.4689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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