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 63675U 26145.36794101 +.00000000 +00000-0 +13073-2 0 00005
2 63675 43.0015 176.0147 0002426 269.6527 90.4063 15.70854820 01
| Epoch (UTC): | 25 May 2026 08:49:50 |
| Eccentricity: | 0.0002426 |
| inclination: | 43.0015° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 176.0147° |
| argument of perigee: | 269.6527° |
| revolutions per day: | 15.70854820 |
| mean anomaly at epoch: | 90.4063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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