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 29268U 26145.61755626 +.00000000 +00000-0 +11617-4 0 00006
2 29268 97.8314 331.1568 0015242 140.5969 311.3119 14.64642002 04
| Epoch (UTC): | 25 May 2026 14:49:16 |
| Eccentricity: | 0.0015242 |
| inclination: | 97.8314° |
| perigee height: | 667 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 331.1568° |
| argument of perigee: | 140.5969° |
| revolutions per day: | 14.64642002 |
| mean anomaly at epoch: | 311.3119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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