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 21423U 26022.16429733 +.00000000 +00000-0 +92446-4 0 00001
2 21423 82.4919 263.8201 0018012 37.9941 322.2539 14.81782691 07
| Epoch (UTC): | 22 January 2026 03:56:35 |
| Eccentricity: | 0.0018012 |
| inclination: | 82.4919° |
| perigee height: | 611 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 263.8201° |
| argument of perigee: | 37.9941° |
| revolutions per day: | 14.81782691 |
| mean anomaly at epoch: | 322.2539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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