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 29643U 26145.59372492 +.00000000 +00000-0 +00000-0 0 00006
2 29643 2.7471 80.7571 0001583 340.8115 284.1470 1.00272389 02
| Epoch (UTC): | 25 May 2026 14:14:57 |
| Eccentricity: | 0.0001583 |
| inclination: | 2.7471° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 80.7571° |
| argument of perigee: | 340.8115° |
| revolutions per day: | 1.00272389 |
| mean anomaly at epoch: | 284.1470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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