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 26073.13182301 +.00000000 +00000-0 +39631-3 0 00009
2 39417 97.8156 34.9774 0043050 205.1786 154.7340 15.00372843 04
| Epoch (UTC): | 14 March 2026 03:09:49 |
| Eccentricity: | 0.0043050 |
| inclination: | 97.8156° |
| perigee height: | 536 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 34.9774° |
| argument of perigee: | 205.1786° |
| revolutions per day: | 15.00372843 |
| mean anomaly at epoch: | 154.7340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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