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 65143U 26145.38310067 +.00000000 +00000-0 +98455-3 0 00002
2 65143 51.8993 186.5161 0000992 66.2413 293.8654 14.80025349 09
| Epoch (UTC): | 25 May 2026 09:11:39 |
| Eccentricity: | 0.0000992 |
| inclination: | 51.8993° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 186.5161° |
| argument of perigee: | 66.2413° |
| revolutions per day: | 14.80025349 |
| mean anomaly at epoch: | 293.8654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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