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 26029.83239045 +.00000000 +00000-0 +00000-0 0 00008
2 39172 0.0621 276.6001 0002607 27.9515 83.6685 1.00270615 07
| Epoch (UTC): | 29 January 2026 19:58:38 |
| Eccentricity: | 0.0002607 |
| inclination: | 0.0621° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 276.6001° |
| argument of perigee: | 27.9515° |
| revolutions per day: | 1.00270615 |
| mean anomaly at epoch: | 83.6685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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