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 26088.15602700 +.00000000 +00000-0 +65455-4 0 00009
2 21090 82.9252 9.9039 0021939 70.8411 289.5118 13.76672716 07
| Epoch (UTC): | 29 March 2026 03:44:40 |
| Eccentricity: | 0.0021939 |
| inclination: | 82.9252° |
| perigee height: | 960 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 9.9039° |
| argument of perigee: | 70.8411° |
| revolutions per day: | 13.76672716 |
| mean anomaly at epoch: | 289.5118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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