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 65286U 26145.40471999 +.00000000 +00000-0 +18839-3 0 00003
2 65286 97.4459 197.8974 0002390 124.4675 235.6778 15.05653629 05
| Epoch (UTC): | 25 May 2026 09:42:47 |
| Eccentricity: | 0.0002390 |
| inclination: | 97.4459° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 197.8974° |
| argument of perigee: | 124.4675° |
| revolutions per day: | 15.05653629 |
| mean anomaly at epoch: | 235.6778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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