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 39441U 26150.77596801 +.00000000 +00000-0 +31567-3 0 00006
2 39441 97.8892 90.1171 0067433 125.9933 234.7560 14.86539554 07
| Epoch (UTC): | 30 May 2026 18:37:23 |
| Eccentricity: | 0.0067433 |
| inclination: | 97.8892° |
| perigee height: | 562 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 90.1171° |
| argument of perigee: | 125.9933° |
| revolutions per day: | 14.86539554 |
| mean anomaly at epoch: | 234.7560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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