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 47504U 26144.96308579 +.00000000 +00000-0 +25671-3 0 00001
2 47504 97.1127 147.3969 0010736 189.7487 170.3554 15.43388479 06
| Epoch (UTC): | 24 May 2026 23:06:50 |
| Eccentricity: | 0.0010736 |
| inclination: | 97.1127° |
| perigee height: | 429 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 147.3969° |
| argument of perigee: | 189.7487° |
| revolutions per day: | 15.43388479 |
| mean anomaly at epoch: | 170.3554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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