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 61669U 26145.14543265 +.00000000 +00000-0 +12839-4 0 00006
2 61669 53.1600 93.6581 0001207 89.7987 270.3152 15.30196760 03
| Epoch (UTC): | 25 May 2026 03:29:25 |
| Eccentricity: | 0.0001207 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 93.6581° |
| argument of perigee: | 89.7987° |
| revolutions per day: | 15.30196760 |
| mean anomaly at epoch: | 270.3152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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