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 62954U 26145.58335647 +.00000000 +00000-0 +68518-3 0 00009
2 62954 53.1597 232.6244 0001338 69.0529 87.5527 15.34376125 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001338 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 232.6244° |
| argument of perigee: | 69.0529° |
| revolutions per day: | 15.34376125 |
| mean anomaly at epoch: | 87.5527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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