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 00011U 26134.57973255 +.00000000 +00000-0 +43539-3 0 00001
2 00011 32.8718 212.3460 1445018 225.6562 121.6311 11.90423645 02
| Epoch (UTC): | 14 May 2026 13:54:48 |
| Eccentricity: | 0.1445018 |
| inclination: | 32.8718° |
| perigee height: | 553 km |
| apogee height: | 2895 km |
| right ascension of ascending node: | 212.3460° |
| argument of perigee: | 225.6562° |
| revolutions per day: | 11.90423645 |
| mean anomaly at epoch: | 121.6311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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