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 48356U 26145.62334830 +.00000000 +00000-0 +13013-3 0 00007
2 48356 53.1606 0.5811 0001940 80.9893 279.1328 15.31708986 05
| Epoch (UTC): | 25 May 2026 14:57:37 |
| Eccentricity: | 0.0001940 |
| inclination: | 53.1606° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 0.5811° |
| argument of perigee: | 80.9893° |
| revolutions per day: | 15.31708986 |
| mean anomaly at epoch: | 279.1328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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