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 62476U 26145.46875589 +.00000000 +00000-0 +70310-3 0 00002
2 62476 42.9988 302.9089 0001071 278.5116 81.5614 15.27595182 07
| Epoch (UTC): | 25 May 2026 11:15:00 |
| Eccentricity: | 0.0001071 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.9089° |
| argument of perigee: | 278.5116° |
| revolutions per day: | 15.27595182 |
| mean anomaly at epoch: | 81.5614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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