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 63830U 26145.24405666 +.00000000 +00000-0 +76442-3 0 00000
2 63830 43.0005 100.1108 0001029 274.2525 85.8209 15.27590181 05
| Epoch (UTC): | 25 May 2026 05:51:26 |
| Eccentricity: | 0.0001029 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.1108° |
| argument of perigee: | 274.2525° |
| revolutions per day: | 15.27590181 |
| mean anomaly at epoch: | 85.8209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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