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 48074U 26145.39691976 +.00000000 +00000-0 +55951-3 0 00002
2 48074 87.8944 324.7614 0001786 99.3368 260.7964 13.13469838 02
| Epoch (UTC): | 25 May 2026 09:31:33 |
| Eccentricity: | 0.0001786 |
| inclination: | 87.8944° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7614° |
| argument of perigee: | 99.3368° |
| revolutions per day: | 13.13469838 |
| mean anomaly at epoch: | 260.7964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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