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 63819U 26145.26473682 +.00000000 +00000-0 +59029-3 0 00004
2 63819 43.0001 100.2506 0001463 255.3551 104.7139 15.28212870 02
| Epoch (UTC): | 25 May 2026 06:21:13 |
| Eccentricity: | 0.0001463 |
| inclination: | 43.0001° |
| perigee height: | 480 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 100.2506° |
| argument of perigee: | 255.3551° |
| revolutions per day: | 15.28212870 |
| mean anomaly at epoch: | 104.7139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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