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 47844U 26145.54793689 +.00000000 +00000-0 +42776-4 0 00009
2 47844 53.1620 248.4432 0001768 97.0224 263.0978 15.31027394 09
| Epoch (UTC): | 25 May 2026 13:09:01 |
| Eccentricity: | 0.0001768 |
| inclination: | 53.1620° |
| perigee height: | 472 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 248.4432° |
| argument of perigee: | 97.0224° |
| revolutions per day: | 15.31027394 |
| mean anomaly at epoch: | 263.0978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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