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 26410U 26152.52173265 +.00000000 +00000-0 +00000-0 0 00003
2 26410 149.8860 47.8948 9033309 264.9086 0.0606 0.44869700 03
| Epoch (UTC): | 01 June 2026 12:31:17 |
| Eccentricity: | 0.9033309 |
| inclination: | 149.8860° |
| perigee height: | 589 km |
| apogee height: | 130799 km |
| right ascension of ascending node: | 47.8948° |
| argument of perigee: | 264.9086° |
| revolutions per day: | 0.44869700 |
| mean anomaly at epoch: | 0.0606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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