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 26112.19856808 +.00000000 +00000-0 +59209-4 0 00009
2 21089 82.9270 18.8754 0030439 102.1416 61.7758 13.74888340 07
| Epoch (UTC): | 22 April 2026 04:45:56 |
| Eccentricity: | 0.0030439 |
| inclination: | 82.9270° |
| perigee height: | 960 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 18.8754° |
| argument of perigee: | 102.1416° |
| revolutions per day: | 13.74888340 |
| mean anomaly at epoch: | 61.7758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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