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 61933U 26145.22798161 +.00000000 +00000-0 +65512-3 0 00001
2 61933 43.0021 209.8186 0001140 278.6257 81.4466 15.27594822 05
| Epoch (UTC): | 25 May 2026 05:28:17 |
| Eccentricity: | 0.0001140 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 209.8186° |
| argument of perigee: | 278.6257° |
| revolutions per day: | 15.27594822 |
| mean anomaly at epoch: | 81.4466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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