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 39417U 26066.12901183 +.00000000 +00000-0 +43751-3 0 00005
2 39417 97.8183 27.9406 0042138 228.5830 131.1769 15.00291692 09
| Epoch (UTC): | 07 March 2026 03:05:46 |
| Eccentricity: | 0.0042138 |
| inclination: | 97.8183° |
| perigee height: | 537 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 27.9406° |
| argument of perigee: | 228.5830° |
| revolutions per day: | 15.00291692 |
| mean anomaly at epoch: | 131.1769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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