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 62678U 26145.19983086 +.00000000 +00000-0 +35051-3 0 00001
2 62678 97.4017 227.1909 0005569 54.8787 305.2974 15.28847359 05
| Epoch (UTC): | 25 May 2026 04:47:45 |
| Eccentricity: | 0.0005569 |
| inclination: | 97.4017° |
| perigee height: | 475 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 227.1909° |
| argument of perigee: | 54.8787° |
| revolutions per day: | 15.28847359 |
| mean anomaly at epoch: | 305.2974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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