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 62725U 26145.31301287 +.00000000 +00000-0 +33155-3 0 00008
2 62725 97.4229 218.2191 0004901 354.6912 5.4269 15.17754378 09
| Epoch (UTC): | 25 May 2026 07:30:44 |
| Eccentricity: | 0.0004901 |
| inclination: | 97.4229° |
| perigee height: | 509 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 218.2191° |
| argument of perigee: | 354.6912° |
| revolutions per day: | 15.17754378 |
| mean anomaly at epoch: | 5.4269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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