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 18215U 26076.00173641 +.00000000 +00000-0 +47611-4 0 00006
2 18215 82.5144 166.3822 0020206 33.0391 55.5611 14.85644220 09
| Epoch (UTC): | 17 March 2026 00:02:30 |
| Eccentricity: | 0.0020206 |
| inclination: | 82.5144° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 166.3822° |
| argument of perigee: | 33.0391° |
| revolutions per day: | 14.85644220 |
| mean anomaly at epoch: | 55.5611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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