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 21903U 26069.22981199 +.00000000 +00000-0 +66707-4 0 00002
2 21903 82.9412 341.8704 0041942 204.8132 308.9826 13.74743893 05
| Epoch (UTC): | 10 March 2026 05:30:55 |
| Eccentricity: | 0.0041942 |
| inclination: | 82.9412° |
| perigee height: | 952 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 341.8704° |
| argument of perigee: | 204.8132° |
| revolutions per day: | 13.74743893 |
| mean anomaly at epoch: | 308.9826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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