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 61007U 26145.16137201 +.00000000 +00000-0 +47629-4 0 00008
2 61007 53.1626 54.7357 0001242 91.9140 268.2005 15.34395395 03
| Epoch (UTC): | 25 May 2026 03:52:22 |
| Eccentricity: | 0.0001242 |
| inclination: | 53.1626° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 54.7357° |
| argument of perigee: | 91.9140° |
| revolutions per day: | 15.34395395 |
| mean anomaly at epoch: | 268.2005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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