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 63962U 26145.36798198 +.00000000 +00000-0 +91734-3 0 00005
2 63962 42.9998 103.1471 0001282 271.5345 88.5360 15.27595433 00
| Epoch (UTC): | 25 May 2026 08:49:53 |
| Eccentricity: | 0.0001282 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.1471° |
| argument of perigee: | 271.5345° |
| revolutions per day: | 15.27595433 |
| mean anomaly at epoch: | 88.5360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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