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 39030U 26145.49887497 +.00000000 +00000-0 -11763-5 0 00006
2 39030 97.6839 344.0667 0002123 75.9071 284.2375 14.75514611 02
| Epoch (UTC): | 25 May 2026 11:58:22 |
| Eccentricity: | 0.0002123 |
| inclination: | 97.6839° |
| perigee height: | 642 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 344.0667° |
| argument of perigee: | 75.9071° |
| revolutions per day: | 14.75514611 |
| mean anomaly at epoch: | 284.2375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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