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 62477U 26145.49430148 +.00000000 +00000-0 +60789-3 0 00003
2 62477 42.9989 302.2342 0001475 261.0086 99.0598 15.27601507 09
| Epoch (UTC): | 25 May 2026 11:51:47 |
| Eccentricity: | 0.0001475 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.2342° |
| argument of perigee: | 261.0086° |
| revolutions per day: | 15.27601507 |
| mean anomaly at epoch: | 99.0598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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