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 65197U 26145.37841870 +.00000000 +00000-0 +18847-3 0 00008
2 65197 97.4499 17.9255 0002579 81.8672 278.2848 15.05654382 04
| Epoch (UTC): | 25 May 2026 09:04:55 |
| Eccentricity: | 0.0002579 |
| inclination: | 97.4499° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.9255° |
| argument of perigee: | 81.8672° |
| revolutions per day: | 15.05654382 |
| mean anomaly at epoch: | 278.2848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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