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 39266U 26088.12668963 +.00000000 +00000-0 +69700-3 0 00009
2 39266 80.9289 89.1537 0119756 99.2497 262.2333 15.80713528 07
| Epoch (UTC): | 29 March 2026 03:02:25 |
| Eccentricity: | 0.0119756 |
| inclination: | 80.9289° |
| perigee height: | 248 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 89.1537° |
| argument of perigee: | 99.2497° |
| revolutions per day: | 15.80713528 |
| mean anomaly at epoch: | 262.2333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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