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 21689U 26088.17960800 +.00000000 +00000-0 -11405-3 0 00009
2 21689 99.4584 297.4916 0024776 301.0860 58.7873 14.02282235 06
| Epoch (UTC): | 29 March 2026 04:18:38 |
| Eccentricity: | 0.0024776 |
| inclination: | 99.4584° |
| perigee height: | 868 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 297.4916° |
| argument of perigee: | 301.0860° |
| revolutions per day: | 14.02282235 |
| mean anomaly at epoch: | 58.7873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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