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 47797U 26145.33711836 +.00000000 +00000-0 +42961-4 0 00003
2 47797 53.1593 258.8926 0001050 79.7082 280.4038 15.31701668 04
| Epoch (UTC): | 25 May 2026 08:05:27 |
| Eccentricity: | 0.0001050 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 258.8926° |
| argument of perigee: | 79.7082° |
| revolutions per day: | 15.31701668 |
| mean anomaly at epoch: | 280.4038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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