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 29505U 26145.59578633 +.00000000 +00000-0 +38533-3 0 00003
2 29505 97.6376 186.4966 0002560 185.7876 174.3328 15.16637691 09
| Epoch (UTC): | 25 May 2026 14:17:55 |
| Eccentricity: | 0.0002560 |
| inclination: | 97.6376° |
| perigee height: | 514 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 186.4966° |
| argument of perigee: | 185.7876° |
| revolutions per day: | 15.16637691 |
| mean anomaly at epoch: | 174.3328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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