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 26150.54395617 +.00000000 +00000-0 +53141-3 0 00005
2 29505 97.6369 191.4804 0003110 168.6697 191.4606 15.16715347 05
| Epoch (UTC): | 30 May 2026 13:03:17 |
| Eccentricity: | 0.0003110 |
| inclination: | 97.6369° |
| perigee height: | 514 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 191.4804° |
| argument of perigee: | 168.6697° |
| revolutions per day: | 15.16715347 |
| mean anomaly at epoch: | 191.4606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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