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 26071.97411800 +.00000000 +00000-0 +11895-3 0 00005
2 28414 97.6149 91.0873 0006712 104.0399 256.1575 15.05660971 08
| Epoch (UTC): | 12 March 2026 23:22:43 |
| Eccentricity: | 0.0006712 |
| inclination: | 97.6149° |
| perigee height: | 545 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 91.0873° |
| argument of perigee: | 104.0399° |
| revolutions per day: | 15.05660971 |
| mean anomaly at epoch: | 256.1575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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