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 61949U 26145.31076174 +.00000000 +00000-0 +18904-2 0 00003
2 61949 53.1575 353.4321 0001341 85.5313 274.5858 15.69788567 03
| Epoch (UTC): | 25 May 2026 07:27:29 |
| Eccentricity: | 0.0001341 |
| inclination: | 53.1575° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 353.4321° |
| argument of perigee: | 85.5313° |
| revolutions per day: | 15.69788567 |
| mean anomaly at epoch: | 274.5858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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