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 61261U 26145.36649192 +.00000000 +00000-0 -41644-4 0 00001
2 61261 53.1602 197.8493 0001314 82.6297 277.4853 15.30174382 09
| Epoch (UTC): | 25 May 2026 08:47:44 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 197.8493° |
| argument of perigee: | 82.6297° |
| revolutions per day: | 15.30174382 |
| mean anomaly at epoch: | 277.4853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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