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 63662U 26145.58780178 +.00000000 +00000-0 +00000-0 0 00008
2 63662 4.5069 280.0974 0003520 133.8340 61.1928 1.00273322 08
| Epoch (UTC): | 25 May 2026 14:06:26 |
| Eccentricity: | 0.0003520 |
| inclination: | 4.5069° |
| perigee height: | 35771 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 280.0974° |
| argument of perigee: | 133.8340° |
| revolutions per day: | 1.00273322 |
| mean anomaly at epoch: | 61.1928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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