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 26076.19891207 +.00000000 +00000-0 +48511-4 0 00001
2 18215 82.5144 166.1968 0020188 32.4273 30.0786 14.85644419 00
| Epoch (UTC): | 17 March 2026 04:46:26 |
| Eccentricity: | 0.0020188 |
| inclination: | 82.5144° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 166.1968° |
| argument of perigee: | 32.4273° |
| revolutions per day: | 14.85644419 |
| mean anomaly at epoch: | 30.0786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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