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 62953U 26145.23777583 +.00000000 +00000-0 +70625-3 0 00001
2 62953 53.1604 234.3326 0001152 73.1102 287.0027 15.34411040 01
| Epoch (UTC): | 25 May 2026 05:42:23 |
| Eccentricity: | 0.0001152 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 234.3326° |
| argument of perigee: | 73.1102° |
| revolutions per day: | 15.34411040 |
| mean anomaly at epoch: | 287.0027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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