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 26148.05847986 +.00000000 +00000-0 +00000-0 0 00004
2 26410 149.8742 47.2072 9027933 264.1302 0.1148 0.44849367 02
| Epoch (UTC): | 28 May 2026 01:24:12 |
| Eccentricity: | 0.9027933 |
| inclination: | 149.8742° |
| perigee height: | 630 km |
| apogee height: | 130801 km |
| right ascension of ascending node: | 47.2072° |
| argument of perigee: | 264.1302° |
| revolutions per day: | 0.44849367 |
| mean anomaly at epoch: | 0.1148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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