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 65189U 26145.59440315 +.00000000 +00000-0 +25944-3 0 00008
2 65189 97.4505 18.0945 0002276 81.5077 278.6408 15.05657931 00
| Epoch (UTC): | 25 May 2026 14:15:56 |
| Eccentricity: | 0.0002276 |
| inclination: | 97.4505° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 18.0945° |
| argument of perigee: | 81.5077° |
| revolutions per day: | 15.05657931 |
| mean anomaly at epoch: | 278.6408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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