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 47448U 26145.56250056 +.00000000 +00000-0 +19942-3 0 00005
2 47448 97.2352 196.3696 0004980 245.6661 114.4066 15.40595955 08
| Epoch (UTC): | 25 May 2026 13:30:00 |
| Eccentricity: | 0.0004980 |
| inclination: | 97.2352° |
| perigee height: | 441 km |
| apogee height: | 448 km |
| right ascension of ascending node: | 196.3696° |
| argument of perigee: | 245.6661° |
| revolutions per day: | 15.40595955 |
| mean anomaly at epoch: | 114.4066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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