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 47839U 26145.49039056 +.00000000 +00000-0 +86065-5 0 00008
2 47839 53.1595 219.7589 0001232 77.3480 282.7659 15.31703077 02
| Epoch (UTC): | 25 May 2026 11:46:09 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 219.7589° |
| argument of perigee: | 77.3480° |
| revolutions per day: | 15.31703077 |
| mean anomaly at epoch: | 282.7659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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