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 26102.14019248 +.00000000 +00000-0 +26297-3 0 00006
2 39417 97.8126 64.1276 0045030 111.9043 248.6977 15.00655092 02
| Epoch (UTC): | 12 April 2026 03:21:52 |
| Eccentricity: | 0.0045030 |
| inclination: | 97.8126° |
| perigee height: | 534 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 64.1276° |
| argument of perigee: | 111.9043° |
| revolutions per day: | 15.00655092 |
| mean anomaly at epoch: | 248.6977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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