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 61849U 26145.50777036 +.00000000 +00000-0 -20136-5 0 00002
2 61849 42.9995 153.1138 0001006 272.5087 87.5649 15.27574250 05
| Epoch (UTC): | 25 May 2026 12:11:11 |
| Eccentricity: | 0.0001006 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.1138° |
| argument of perigee: | 272.5087° |
| revolutions per day: | 15.27574250 |
| mean anomaly at epoch: | 87.5649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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