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 61065U 26145.55054038 +.00000000 +00000-0 +25817-4 0 00006
2 61065 53.1611 94.2279 0001204 86.3738 273.7401 15.30198797 06
| Epoch (UTC): | 25 May 2026 13:12:46 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 94.2279° |
| argument of perigee: | 86.3738° |
| revolutions per day: | 15.30198797 |
| mean anomaly at epoch: | 273.7401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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