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 62653U 26145.51813154 +.00000000 +00000-0 +15818-3 0 00007
2 62653 97.3956 225.4917 0002905 70.1325 290.0225 15.23372852 05
| Epoch (UTC): | 25 May 2026 12:26:06 |
| Eccentricity: | 0.0002905 |
| inclination: | 97.3956° |
| perigee height: | 494 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 225.4917° |
| argument of perigee: | 70.1325° |
| revolutions per day: | 15.23372852 |
| mean anomaly at epoch: | 290.0225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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