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 28414U 26076.29383175 +.00000000 +00000-0 +14768-3 0 00000
2 28414 97.6134 95.3518 0006786 92.8219 267.3784 15.05684348 01
| Epoch (UTC): | 17 March 2026 07:03:07 |
| Eccentricity: | 0.0006786 |
| inclination: | 97.6134° |
| perigee height: | 545 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 95.3518° |
| argument of perigee: | 92.8219° |
| revolutions per day: | 15.05684348 |
| mean anomaly at epoch: | 267.3784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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