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 63820U 26145.26461477 +.00000000 +00000-0 +50446-3 0 00009
2 63820 43.0007 100.2766 0001545 260.2310 99.8367 15.27592328 02
| Epoch (UTC): | 25 May 2026 06:21:02 |
| Eccentricity: | 0.0001545 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.2766° |
| argument of perigee: | 260.2310° |
| revolutions per day: | 15.27592328 |
| mean anomaly at epoch: | 99.8367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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