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 26135.25070197 +.00000000 +00000-0 +40901-3 0 00000
2 00011 32.8720 209.8069 1445077 229.4736 117.0890 11.90424441 07
| Epoch (UTC): | 15 May 2026 06:01:00 |
| Eccentricity: | 0.1445077 |
| inclination: | 32.8720° |
| perigee height: | 553 km |
| apogee height: | 2895 km |
| right ascension of ascending node: | 209.8069° |
| argument of perigee: | 229.4736° |
| revolutions per day: | 11.90424441 |
| mean anomaly at epoch: | 117.0890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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