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 39769U 26145.50651719 +.00000000 +00000-0 +41242-3 0 00005
2 39769 97.6527 214.4480 0003602 32.2758 327.8684 14.98264511 02
| Epoch (UTC): | 25 May 2026 12:09:23 |
| Eccentricity: | 0.0003602 |
| inclination: | 97.6527° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 214.4480° |
| argument of perigee: | 32.2758° |
| revolutions per day: | 14.98264511 |
| mean anomaly at epoch: | 327.8684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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