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 62714U 26145.50700545 +.00000000 +00000-0 +33907-3 0 00002
2 62714 97.7052 225.9203 0001768 148.9763 211.1564 14.97591838 00
| Epoch (UTC): | 25 May 2026 12:10:05 |
| Eccentricity: | 0.0001768 |
| inclination: | 97.7052° |
| perigee height: | 573 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 225.9203° |
| argument of perigee: | 148.9763° |
| revolutions per day: | 14.97591838 |
| mean anomaly at epoch: | 211.1564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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