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 39152U 26105.81919464 +.00000000 +00000-0 +10793-3 0 00002
2 39152 97.7915 196.9314 0010839 313.1655 46.8659 14.96039208 08
| Epoch (UTC): | 15 April 2026 19:39:38 |
| Eccentricity: | 0.0010839 |
| inclination: | 97.7915° |
| perigee height: | 572 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 196.9314° |
| argument of perigee: | 313.1655° |
| revolutions per day: | 14.96039208 |
| mean anomaly at epoch: | 46.8659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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