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 62667U 26145.50931389 +.00000000 +00000-0 +35795-3 0 00008
2 62667 97.4025 227.4414 0005256 54.8091 305.3641 15.28702642 04
| Epoch (UTC): | 25 May 2026 12:13:24 |
| Eccentricity: | 0.0005256 |
| inclination: | 97.4025° |
| perigee height: | 476 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 227.4414° |
| argument of perigee: | 54.8091° |
| revolutions per day: | 15.28702642 |
| mean anomaly at epoch: | 305.3641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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