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 61969U 26145.26589859 +.00000000 +00000-0 +49948-3 0 00001
2 61969 43.0013 100.2413 0001739 269.5275 90.5378 15.27582965 03
| Epoch (UTC): | 25 May 2026 06:22:53 |
| Eccentricity: | 0.0001739 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.2413° |
| argument of perigee: | 269.5275° |
| revolutions per day: | 15.27582965 |
| mean anomaly at epoch: | 90.5378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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