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 63825U 26145.25562622 +.00000000 +00000-0 +57291-3 0 00002
2 63825 43.0026 100.2077 0001264 263.7505 96.3202 15.27617581 04
| Epoch (UTC): | 25 May 2026 06:08:06 |
| Eccentricity: | 0.0001264 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.2077° |
| argument of perigee: | 263.7505° |
| revolutions per day: | 15.27617581 |
| mean anomaly at epoch: | 96.3202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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