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 47838U 26145.01289647 +.00000000 +00000-0 -19757-4 0 00002
2 47838 53.1593 250.7684 0001270 73.3423 286.7718 15.31692164 09
| Epoch (UTC): | 25 May 2026 00:18:34 |
| Eccentricity: | 0.0001270 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 250.7684° |
| argument of perigee: | 73.3423° |
| revolutions per day: | 15.31692164 |
| mean anomaly at epoch: | 286.7718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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