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 21938U 26075.69671772 +.00000000 +00000-0 +40866-4 0 00009
2 21938 82.9325 148.5596 0027551 278.3233 249.3584 13.75550070 08
| Epoch (UTC): | 16 March 2026 16:43:16 |
| Eccentricity: | 0.0027551 |
| inclination: | 82.9325° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 148.5596° |
| argument of perigee: | 278.3233° |
| revolutions per day: | 13.75550070 |
| mean anomaly at epoch: | 249.3584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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