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 62712U 26144.20091669 +.00000000 +00000-0 +45168-3 0 00008
2 62712 97.7275 227.2920 0001322 233.1803 126.9301 15.03332010 09
| Epoch (UTC): | 24 May 2026 04:49:19 |
| Eccentricity: | 0.0001322 |
| inclination: | 97.7275° |
| perigee height: | 556 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 227.2920° |
| argument of perigee: | 233.1803° |
| revolutions per day: | 15.03332010 |
| mean anomaly at epoch: | 126.9301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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