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 62648U 26145.21279752 +.00000000 +00000-0 +33235-3 0 00001
2 62648 97.3952 227.5746 0003153 86.0460 274.1141 15.30355310 08
| Epoch (UTC): | 25 May 2026 05:06:25 |
| Eccentricity: | 0.0003153 |
| inclination: | 97.3952° |
| perigee height: | 473 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 227.5746° |
| argument of perigee: | 86.0460° |
| revolutions per day: | 15.30355310 |
| mean anomaly at epoch: | 274.1141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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