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 21397U 26073.66610946 +.00000000 +00000-0 +29890-3 0 00002
2 21397 82.5202 332.0231 0013489 318.7791 41.2416 15.04847916 01
| Epoch (UTC): | 14 March 2026 15:59:11 |
| Eccentricity: | 0.0013489 |
| inclination: | 82.5202° |
| perigee height: | 543 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 332.0231° |
| argument of perigee: | 318.7791° |
| revolutions per day: | 15.04847916 |
| mean anomaly at epoch: | 41.2416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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