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 29507U 26159.02283543 +.00000000 +00000-0 +22885-3 0 00004
2 29507 97.5454 203.6582 0031417 316.1729 43.7012 15.17717799 01
| Epoch (UTC): | 08 June 2026 00:32:52 |
| Eccentricity: | 0.0031417 |
| inclination: | 97.5454° |
| perigee height: | 491 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 203.6582° |
| argument of perigee: | 316.1729° |
| revolutions per day: | 15.17717799 |
| mean anomaly at epoch: | 43.7012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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