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 29495U 26145.54259935 +.00000000 +00000-0 +00000-0 0 00002
2 29495 2.9790 79.9236 0003764 339.4502 171.0731 1.00272093 04
| Epoch (UTC): | 25 May 2026 13:01:20 |
| Eccentricity: | 0.0003764 |
| inclination: | 2.9790° |
| perigee height: | 35771 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 79.9236° |
| argument of perigee: | 339.4502° |
| revolutions per day: | 1.00272093 |
| mean anomaly at epoch: | 171.0731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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