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 26153.06456104 +.00000000 +00000-0 +25754-3 0 00003
2 39441 97.8894 92.3889 0067561 118.6235 242.1799 14.86551470 03
| Epoch (UTC): | 02 June 2026 01:32:58 |
| Eccentricity: | 0.0067561 |
| inclination: | 97.8894° |
| perigee height: | 562 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 92.3889° |
| argument of perigee: | 118.6235° |
| revolutions per day: | 14.86551470 |
| mean anomaly at epoch: | 242.1799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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