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 39267U 26145.16209154 +.00000000 +00000-0 +27909-3 0 00006
2 39267 80.9895 198.2501 0463473 354.4720 5.1460 14.79361735 08
| Epoch (UTC): | 25 May 2026 03:53:24 |
| Eccentricity: | 0.0463473 |
| inclination: | 80.9895° |
| perigee height: | 306 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 198.2501° |
| argument of perigee: | 354.4720° |
| revolutions per day: | 14.79361735 |
| mean anomaly at epoch: | 5.1460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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