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 63821U 26109.23284796 +.00000000 +00000-0 +73078-3 0 00000
2 63821 43.0005 303.7113 0001771 283.6299 76.4355 15.27598957 05
| Epoch (UTC): | 19 April 2026 05:35:18 |
| Eccentricity: | 0.0001771 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 303.7113° |
| argument of perigee: | 283.6299° |
| revolutions per day: | 15.27598957 |
| mean anomaly at epoch: | 76.4355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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