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 61005U 26145.52309175 +.00000000 +00000-0 +19747-4 0 00007
2 61005 53.1604 68.7299 0001280 84.7517 275.3629 15.30192814 05
| Epoch (UTC): | 25 May 2026 12:33:15 |
| Eccentricity: | 0.0001280 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 68.7299° |
| argument of perigee: | 84.7517° |
| revolutions per day: | 15.30192814 |
| mean anomaly at epoch: | 275.3629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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