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 62622U 26145.15354544 +.00000000 +00000-0 +33142-3 0 00006
2 62622 97.3960 226.2803 0005674 60.3997 299.7807 15.27596118 00
| Epoch (UTC): | 25 May 2026 03:41:06 |
| Eccentricity: | 0.0005674 |
| inclination: | 97.3960° |
| perigee height: | 479 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 226.2803° |
| argument of perigee: | 60.3997° |
| revolutions per day: | 15.27596118 |
| mean anomaly at epoch: | 299.7807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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