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 21089U 26087.94500161 +.00000000 +00000-0 +40049-4 0 00003
2 21089 82.9249 36.8813 0029252 167.8039 258.4311 13.74885979 04
| Epoch (UTC): | 28 March 2026 22:40:48 |
| Eccentricity: | 0.0029252 |
| inclination: | 82.9249° |
| perigee height: | 961 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 36.8813° |
| argument of perigee: | 167.8039° |
| revolutions per day: | 13.74885979 |
| mean anomaly at epoch: | 258.4311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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