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 62612U 26145.49957573 +.00000000 +00000-0 +32801-3 0 00004
2 62612 97.4020 227.6824 0001893 81.5947 278.5508 15.28167941 06
| Epoch (UTC): | 25 May 2026 11:59:23 |
| Eccentricity: | 0.0001893 |
| inclination: | 97.4020° |
| perigee height: | 480 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 227.6824° |
| argument of perigee: | 81.5947° |
| revolutions per day: | 15.28167941 |
| mean anomaly at epoch: | 278.5508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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