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 39172U 26145.50439168 +.00000000 +00000-0 +00000-0 0 00009
2 39172 0.0263 307.4239 0002661 121.5604 315.1869 1.00271465 06
| Epoch (UTC): | 25 May 2026 12:06:19 |
| Eccentricity: | 0.0002661 |
| inclination: | 0.0263° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 307.4239° |
| argument of perigee: | 121.5604° |
| revolutions per day: | 1.00271465 |
| mean anomaly at epoch: | 315.1869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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