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 48075U 26145.41568080 +.00000000 +00000-0 +79319-3 0 00009
2 48075 87.8931 324.7737 0001493 91.4601 268.6699 13.13470805 01
| Epoch (UTC): | 25 May 2026 09:58:34 |
| Eccentricity: | 0.0001493 |
| inclination: | 87.8931° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7737° |
| argument of perigee: | 91.4601° |
| revolutions per day: | 13.13470805 |
| mean anomaly at epoch: | 268.6699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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