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 39197U 26145.26857479 +.00000000 +00000-0 +11431-3 0 00001
2 39197 97.9345 344.6170 0025330 36.7938 323.5010 14.85830628 01
| Epoch (UTC): | 25 May 2026 06:26:44 |
| Eccentricity: | 0.0025330 |
| inclination: | 97.9345° |
| perigee height: | 593 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 344.6170° |
| argument of perigee: | 36.7938° |
| revolutions per day: | 14.85830628 |
| mean anomaly at epoch: | 323.5010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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