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 63840U 26145.32890913 +.00000000 +00000-0 +66366-3 0 00007
2 63840 43.0054 5.0276 0001541 250.1364 109.9322 15.27597046 03
| Epoch (UTC): | 25 May 2026 07:53:37 |
| Eccentricity: | 0.0001541 |
| inclination: | 43.0054° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.0276° |
| argument of perigee: | 250.1364° |
| revolutions per day: | 15.27597046 |
| mean anomaly at epoch: | 109.9322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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