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 63760U 26145.39746444 +.00000000 +00000-0 +13809-2 0 00007
2 63760 43.0010 189.5145 0002280 259.4796 100.5815 15.70924689 00
| Epoch (UTC): | 25 May 2026 09:32:20 |
| Eccentricity: | 0.0002280 |
| inclination: | 43.0010° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 189.5145° |
| argument of perigee: | 259.4796° |
| revolutions per day: | 15.70924689 |
| mean anomaly at epoch: | 100.5815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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