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 62602U 26145.44116175 +.00000000 +00000-0 +82192-3 0 00001
2 62602 43.0012 204.3702 0002146 276.3184 83.7423 15.27589576 02
| Epoch (UTC): | 25 May 2026 10:35:16 |
| Eccentricity: | 0.0002146 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.3702° |
| argument of perigee: | 276.3184° |
| revolutions per day: | 15.27589576 |
| mean anomaly at epoch: | 83.7423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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