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 61850U 26145.39995685 +.00000000 +00000-0 +45881-4 0 00005
2 61850 43.0012 164.4124 0001130 277.5136 82.5587 15.27580926 00
| Epoch (UTC): | 25 May 2026 09:35:56 |
| Eccentricity: | 0.0001130 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.4124° |
| argument of perigee: | 277.5136° |
| revolutions per day: | 15.27580926 |
| mean anomaly at epoch: | 82.5587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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