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 48924U 26145.60627615 +.00000000 +00000-0 +71477-3 0 00000
2 48924 97.6851 341.2244 0003801 68.8146 291.3523 15.72685822 01
| Epoch (UTC): | 25 May 2026 14:33:02 |
| Eccentricity: | 0.0003801 |
| inclination: | 97.6851° |
| perigee height: | 349 km |
| apogee height: | 354 km |
| right ascension of ascending node: | 341.2244° |
| argument of perigee: | 68.8146° |
| revolutions per day: | 15.72685822 |
| mean anomaly at epoch: | 291.3523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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