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 48696U 26145.23537089 +.00000000 +00000-0 +15905-4 0 00005
2 48696 53.1590 92.5732 0001448 92.7894 267.3273 15.31694719 08
| Epoch (UTC): | 25 May 2026 05:38:56 |
| Eccentricity: | 0.0001448 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 92.5732° |
| argument of perigee: | 92.7894° |
| revolutions per day: | 15.31694719 |
| mean anomaly at epoch: | 267.3273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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