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 62605U 26145.55779513 +.00000000 +00000-0 +96212-3 0 00005
2 62605 43.0026 203.5287 0002311 264.1774 95.8815 15.27597876 04
| Epoch (UTC): | 25 May 2026 13:23:13 |
| Eccentricity: | 0.0002311 |
| inclination: | 43.0026° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 203.5287° |
| argument of perigee: | 264.1774° |
| revolutions per day: | 15.27597876 |
| mean anomaly at epoch: | 95.8815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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