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 26044.86930795 +.00000000 +00000-0 +13720-3 0 00003
2 21422 82.4956 106.6558 0013628 135.4498 224.7824 15.00013558 09
| Epoch (UTC): | 13 February 2026 20:51:48 |
| Eccentricity: | 0.0013628 |
| inclination: | 82.4956° |
| perigee height: | 557 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 106.6558° |
| argument of perigee: | 135.4498° |
| revolutions per day: | 15.00013558 |
| mean anomaly at epoch: | 224.7824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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