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 65962U 26145.35538176 +.00000000 +00000-0 +13622-2 0 00003
2 65962 51.9019 9.1342 0001218 63.9251 296.1836 14.80098737 04
| Epoch (UTC): | 25 May 2026 08:31:44 |
| Eccentricity: | 0.0001218 |
| inclination: | 51.9019° |
| perigee height: | 628 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 9.1342° |
| argument of perigee: | 63.9251° |
| revolutions per day: | 14.80098737 |
| mean anomaly at epoch: | 296.1836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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