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 39428U 26154.99260154 +.00000000 +00000-0 +62312-3 0 00000
2 39428 97.8344 75.3173 0072729 250.1592 109.1778 14.94943245 08
| Epoch (UTC): | 03 June 2026 23:49:20 |
| Eccentricity: | 0.0072729 |
| inclination: | 97.8344° |
| perigee height: | 532 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 75.3173° |
| argument of perigee: | 250.1592° |
| revolutions per day: | 14.94943245 |
| mean anomaly at epoch: | 109.1778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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