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 47804U 26145.53146537 +.00000000 +00000-0 +34497-4 0 00009
2 47804 53.1579 232.7822 0001088 79.2546 280.8578 15.31704966 01
| Epoch (UTC): | 25 May 2026 12:45:18 |
| Eccentricity: | 0.0001088 |
| inclination: | 53.1579° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 232.7822° |
| argument of perigee: | 79.2546° |
| revolutions per day: | 15.31704966 |
| mean anomaly at epoch: | 280.8578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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