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 61676U 26145.14857311 +.00000000 +00000-0 +49753-4 0 00009
2 61676 53.1625 95.0966 0001336 91.3387 268.7768 15.34393664 07
| Epoch (UTC): | 25 May 2026 03:33:56 |
| Eccentricity: | 0.0001336 |
| inclination: | 53.1625° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 95.0966° |
| argument of perigee: | 91.3387° |
| revolutions per day: | 15.34393664 |
| mean anomaly at epoch: | 268.7768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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