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 26130.20383917 +.00000000 +00000-0 +00000-0 0 00000
2 39172 0.0208 346.9581 0002561 81.8354 192.1150 1.00270460 02
| Epoch (UTC): | 10 May 2026 04:53:31 |
| Eccentricity: | 0.0002561 |
| inclination: | 0.0208° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 346.9581° |
| argument of perigee: | 81.8354° |
| revolutions per day: | 1.00270460 |
| mean anomaly at epoch: | 192.1150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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