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 47830U 26145.36044949 +.00000000 +00000-0 +53851-4 0 00008
2 47830 53.1612 259.0154 0001664 87.8756 272.2436 15.31708004 01
| Epoch (UTC): | 25 May 2026 08:39:02 |
| Eccentricity: | 0.0001664 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 259.0154° |
| argument of perigee: | 87.8756° |
| revolutions per day: | 15.31708004 |
| mean anomaly at epoch: | 272.2436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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