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 26088.13690990 +.00000000 +00000-0 +40731-3 0 00006
2 39417 97.8137 50.0550 0044615 156.4937 203.8338 15.00497521 02
| Epoch (UTC): | 29 March 2026 03:17:09 |
| Eccentricity: | 0.0044615 |
| inclination: | 97.8137° |
| perigee height: | 534 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 50.0550° |
| argument of perigee: | 156.4937° |
| revolutions per day: | 15.00497521 |
| mean anomaly at epoch: | 203.8338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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