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 61258U 26145.58335647 +.00000000 +00000-0 +18727-2 0 00001
2 61258 53.1591 196.8018 0000935 74.7402 62.7428 15.34356845 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000935 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 196.8018° |
| argument of perigee: | 74.7402° |
| revolutions per day: | 15.34356845 |
| mean anomaly at epoch: | 62.7428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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