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 21047U 26033.19963970 +.00000000 +00000-0 +00000-0 0 00005
2 21047 13.0370 355.5577 0006442 253.0504 295.0054 0.98285385 05
| Epoch (UTC): | 02 February 2026 04:47:28 |
| Eccentricity: | 0.0006442 |
| inclination: | 13.0370° |
| perigee height: | 36325 km |
| apogee height: | 36380 km |
| right ascension of ascending node: | 355.5577° |
| argument of perigee: | 253.0504° |
| revolutions per day: | 0.98285385 |
| mean anomaly at epoch: | 295.0054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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