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 62498U 26145.46547741 +.00000000 +00000-0 +51344-3 0 00008
2 62498 43.0018 215.3615 0001941 282.4341 77.6294 15.27591403 01
| Epoch (UTC): | 25 May 2026 11:10:17 |
| Eccentricity: | 0.0001941 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.3615° |
| argument of perigee: | 282.4341° |
| revolutions per day: | 15.27591403 |
| mean anomaly at epoch: | 77.6294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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