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 61256U 26145.43495398 +.00000000 +00000-0 +10228-4 0 00003
2 61256 53.1602 197.5653 0001094 73.7395 286.3726 15.30193491 03
| Epoch (UTC): | 25 May 2026 10:26:20 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 197.5653° |
| argument of perigee: | 73.7395° |
| revolutions per day: | 15.30193491 |
| mean anomaly at epoch: | 286.3726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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