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 63763U 26145.54147170 +.00000000 +00000-0 +13358-2 0 00007
2 63763 43.0009 188.8824 0001546 277.6118 82.4574 15.70881519 05
| Epoch (UTC): | 25 May 2026 12:59:43 |
| Eccentricity: | 0.0001546 |
| inclination: | 43.0009° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 188.8824° |
| argument of perigee: | 277.6118° |
| revolutions per day: | 15.70881519 |
| mean anomaly at epoch: | 82.4574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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