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 48060U 26145.20901407 +.00000000 +00000-0 -38104-3 0 00002
2 48060 87.8943 324.8041 0002164 72.6120 287.5246 13.13469484 09
| Epoch (UTC): | 25 May 2026 05:00:58 |
| Eccentricity: | 0.0002164 |
| inclination: | 87.8943° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.8041° |
| argument of perigee: | 72.6120° |
| revolutions per day: | 13.13469484 |
| mean anomaly at epoch: | 287.5246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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