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 26069.80943676 +.00000000 +00000-0 +31097-3 0 00004
2 21397 82.5193 335.7590 0013858 333.9632 26.0896 15.04815448 09
| Epoch (UTC): | 10 March 2026 19:25:35 |
| Eccentricity: | 0.0013858 |
| inclination: | 82.5193° |
| perigee height: | 542 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 335.7590° |
| argument of perigee: | 333.9632° |
| revolutions per day: | 15.04815448 |
| mean anomaly at epoch: | 26.0896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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