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 47826U 26145.00817912 +.00000000 +00000-0 -58267-4 0 00009
2 47826 53.1614 250.4214 0000332 93.9566 266.1474 15.31699623 08
| Epoch (UTC): | 25 May 2026 00:11:46 |
| Eccentricity: | 0.0000332 |
| inclination: | 53.1614° |
| perigee height: | 471 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 250.4214° |
| argument of perigee: | 93.9566° |
| revolutions per day: | 15.31699623 |
| mean anomaly at epoch: | 266.1474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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