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 39427U 26075.83186206 +.00000000 +00000-0 +24252-3 0 00000
2 39427 97.8291 347.7574 0090716 174.3800 185.8453 14.81236910 05
| Epoch (UTC): | 16 March 2026 19:57:52 |
| Eccentricity: | 0.0090716 |
| inclination: | 97.8291° |
| perigee height: | 562 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 347.7574° |
| argument of perigee: | 174.3800° |
| revolutions per day: | 14.81236910 |
| mean anomaly at epoch: | 185.8453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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