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 39173U 26139.48435010 +.00000000 +00000-0 +00000-0 0 00002
2 39173 28.5292 309.6409 7664474 190.5392 130.9181 1.10514254 07
| Epoch (UTC): | 19 May 2026 11:37:27 |
| Eccentricity: | 0.7664474 |
| inclination: | 28.5292° |
| perigee height: | 2851 km |
| apogee height: | 63427 km |
| right ascension of ascending node: | 309.6409° |
| argument of perigee: | 190.5392° |
| revolutions per day: | 1.10514254 |
| mean anomaly at epoch: | 130.9181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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