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 26072.97098124 +.00000000 +00000-0 +11612-3 0 00003
2 28414 97.6147 92.0716 0006787 101.7171 258.4817 15.05666414 09
| Epoch (UTC): | 13 March 2026 23:18:12 |
| Eccentricity: | 0.0006787 |
| inclination: | 97.6147° |
| perigee height: | 545 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 92.0716° |
| argument of perigee: | 101.7171° |
| revolutions per day: | 15.05666414 |
| mean anomaly at epoch: | 258.4817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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