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 26069.14448523 +.00000000 +00000-0 +32585-3 0 00005
2 21397 82.5191 336.4029 0013917 336.6290 23.4302 15.04809379 07
| Epoch (UTC): | 10 March 2026 03:28:03 |
| Eccentricity: | 0.0013917 |
| inclination: | 82.5191° |
| perigee height: | 542 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 336.4029° |
| argument of perigee: | 336.6290° |
| revolutions per day: | 15.04809379 |
| mean anomaly at epoch: | 23.4302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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