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 26052U 26145.73934308 +.00000000 +00000-0 +00000-0 0 00003
2 26052 11.8716 32.6287 0006044 21.2390 161.3118 0.99108542 09
| Epoch (UTC): | 25 May 2026 17:44:39 |
| Eccentricity: | 0.0006044 |
| inclination: | 11.8716° |
| perigee height: | 36090 km |
| apogee height: | 36142 km |
| right ascension of ascending node: | 32.6287° |
| argument of perigee: | 21.2390° |
| revolutions per day: | 0.99108542 |
| mean anomaly at epoch: | 161.3118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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