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 62967U 26145.54509635 +.00000000 +00000-0 +74781-3 0 00008
2 62967 53.1583 234.8188 0000974 74.7748 285.3362 15.34403311 02
| Epoch (UTC): | 25 May 2026 13:04:56 |
| Eccentricity: | 0.0000974 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 234.8188° |
| argument of perigee: | 74.7748° |
| revolutions per day: | 15.34403311 |
| mean anomaly at epoch: | 285.3362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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