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 63841U 26145.02125433 +.00000000 +00000-0 +66774-3 0 00006
2 63841 43.0017 7.0373 0001789 280.8488 79.2163 15.27602001 04
| Epoch (UTC): | 25 May 2026 00:30:36 |
| Eccentricity: | 0.0001789 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 7.0373° |
| argument of perigee: | 280.8488° |
| revolutions per day: | 15.27602001 |
| mean anomaly at epoch: | 79.2163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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