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 62922U 26145.45590720 +.00000000 +00000-0 +48028-3 0 00009
2 62922 43.0045 55.2512 0001004 279.0212 81.0526 15.27588467 02
| Epoch (UTC): | 25 May 2026 10:56:30 |
| Eccentricity: | 0.0001004 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 55.2512° |
| argument of perigee: | 279.0212° |
| revolutions per day: | 15.27588467 |
| mean anomaly at epoch: | 81.0526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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