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 21090U 26022.45303313 +.00000000 +00000-0 +15310-3 0 00002
2 21090 82.9181 58.8722 0019236 252.1804 107.7255 13.76658590 05
| Epoch (UTC): | 22 January 2026 10:52:22 |
| Eccentricity: | 0.0019236 |
| inclination: | 82.9181° |
| perigee height: | 962 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 58.8722° |
| argument of perigee: | 252.1804° |
| revolutions per day: | 13.76658590 |
| mean anomaly at epoch: | 107.7255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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