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 63276U 26145.61215762 +.00000000 +00000-0 +12593-2 0 00007
2 63276 43.0064 8.9045 0011835 284.8194 75.1363 15.70949920 04
| Epoch (UTC): | 25 May 2026 14:41:30 |
| Eccentricity: | 0.0011835 |
| inclination: | 43.0064° |
| perigee height: | 348 km |
| apogee height: | 364 km |
| right ascension of ascending node: | 8.9045° |
| argument of perigee: | 284.8194° |
| revolutions per day: | 15.70949920 |
| mean anomaly at epoch: | 75.1363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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