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 26067.75700889 +.00000000 +00000-0 +75403-4 0 00004
2 21938 82.9338 154.4539 0027711 301.5290 171.0461 13.75549389 01
| Epoch (UTC): | 08 March 2026 18:10:05 |
| Eccentricity: | 0.0027711 |
| inclination: | 82.9338° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 154.4539° |
| argument of perigee: | 301.5290° |
| revolutions per day: | 13.75549389 |
| mean anomaly at epoch: | 171.0461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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