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 62629U 26145.46539719 +.00000000 +00000-0 +37268-3 0 00009
2 62629 97.3925 227.0394 0003787 66.7303 293.4335 15.28798217 08
| Epoch (UTC): | 25 May 2026 11:10:10 |
| Eccentricity: | 0.0003787 |
| inclination: | 97.3925° |
| perigee height: | 477 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 227.0394° |
| argument of perigee: | 66.7303° |
| revolutions per day: | 15.28798217 |
| mean anomaly at epoch: | 293.4335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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