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 62302U 26145.56923509 +.00000000 +00000-0 +32438-3 0 00006
2 62302 53.1575 194.6061 0001102 78.9743 281.1382 15.30202869 01
| Epoch (UTC): | 25 May 2026 13:39:41 |
| Eccentricity: | 0.0001102 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 194.6061° |
| argument of perigee: | 78.9743° |
| revolutions per day: | 15.30202869 |
| mean anomaly at epoch: | 281.1382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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