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 47656U 26145.44982493 +.00000000 +00000-0 +15830-3 0 00002
2 47656 53.1605 52.5024 0001470 90.4526 269.6644 15.31714974 05
| Epoch (UTC): | 25 May 2026 10:47:44 |
| Eccentricity: | 0.0001470 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 52.5024° |
| argument of perigee: | 90.4526° |
| revolutions per day: | 15.31714974 |
| mean anomaly at epoch: | 269.6644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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