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 39211U 26110.50847541 +.00000000 +00000-0 +26251-3 0 00002
2 39211 97.9622 29.3723 0068615 120.1568 240.6497 15.36669802 06
| Epoch (UTC): | 20 April 2026 12:12:12 |
| Eccentricity: | 0.0068615 |
| inclination: | 97.9622° |
| perigee height: | 409 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 29.3723° |
| argument of perigee: | 120.1568° |
| revolutions per day: | 15.36669802 |
| mean anomaly at epoch: | 240.6497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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