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 61069U 26145.14321230 +.00000000 +00000-0 +29817-4 0 00000
2 61069 53.1620 95.9516 0001284 83.8227 276.2921 15.31705155 03
| Epoch (UTC): | 25 May 2026 03:26:13 |
| Eccentricity: | 0.0001284 |
| inclination: | 53.1620° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.9516° |
| argument of perigee: | 83.8227° |
| revolutions per day: | 15.31705155 |
| mean anomaly at epoch: | 276.2921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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