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 61931U 26145.44199250 +.00000000 +00000-0 +57044-3 0 00008
2 61931 43.0022 208.0020 0001977 281.1346 78.9283 15.27615863 05
| Epoch (UTC): | 25 May 2026 10:36:28 |
| Eccentricity: | 0.0001977 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 208.0020° |
| argument of perigee: | 281.1346° |
| revolutions per day: | 15.27615863 |
| mean anomaly at epoch: | 78.9283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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