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 62305U 26145.39800273 +.00000000 +00000-0 +15891-3 0 00006
2 62305 53.1592 197.2403 0001160 94.7644 265.3489 15.30196959 06
| Epoch (UTC): | 25 May 2026 09:33:07 |
| Eccentricity: | 0.0001160 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 197.2403° |
| argument of perigee: | 94.7644° |
| revolutions per day: | 15.30196959 |
| mean anomaly at epoch: | 265.3489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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