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 26072.46490286 +.00000000 +00000-0 +36825-3 0 00000
2 39417 97.8158 34.3075 0042994 207.4020 152.4936 15.00365828 07
| Epoch (UTC): | 13 March 2026 11:09:27 |
| Eccentricity: | 0.0042994 |
| inclination: | 97.8158° |
| perigee height: | 536 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 34.3075° |
| argument of perigee: | 207.4020° |
| revolutions per day: | 15.00365828 |
| mean anomaly at epoch: | 152.4936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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