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 21422U 26159.12332455 +.00000000 +00000-0 +10952-3 0 00002
2 21422 82.4962 356.4290 0013720 111.0853 249.1840 15.00412803 07
| Epoch (UTC): | 08 June 2026 02:57:35 |
| Eccentricity: | 0.0013720 |
| inclination: | 82.4962° |
| perigee height: | 556 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 356.4290° |
| argument of perigee: | 111.0853° |
| revolutions per day: | 15.00412803 |
| mean anomaly at epoch: | 249.1840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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