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 26074.19805801 +.00000000 +00000-0 +25362-3 0 00007
2 21397 82.5203 331.5079 0013433 316.7303 43.2868 15.04850927 01
| Epoch (UTC): | 15 March 2026 04:45:12 |
| Eccentricity: | 0.0013433 |
| inclination: | 82.5203° |
| perigee height: | 543 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 331.5079° |
| argument of perigee: | 316.7303° |
| revolutions per day: | 15.04850927 |
| mean anomaly at epoch: | 43.2868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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