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 63487U 26145.44220241 +.00000000 +00000-0 +26676-3 0 00008
2 63487 43.0014 186.4205 0001321 268.9145 91.1555 15.27560161 00
| Epoch (UTC): | 25 May 2026 10:36:46 |
| Eccentricity: | 0.0001321 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.4205° |
| argument of perigee: | 268.9145° |
| revolutions per day: | 15.27560161 |
| mean anomaly at epoch: | 91.1555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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