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 61260U 26145.55924971 +.00000000 +00000-0 +45827-4 0 00008
2 61260 53.1601 196.9188 0001147 86.5470 273.5662 15.30196131 09
| Epoch (UTC): | 25 May 2026 13:25:19 |
| Eccentricity: | 0.0001147 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 196.9188° |
| argument of perigee: | 86.5470° |
| revolutions per day: | 15.30196131 |
| mean anomaly at epoch: | 273.5662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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