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 62010U 26145.66096384 +.00000000 +00000-0 +20842-2 0 00000
2 62010 53.1581 21.8740 0000726 140.0755 220.0317 15.69879716 07
| Epoch (UTC): | 25 May 2026 15:51:47 |
| Eccentricity: | 0.0000726 |
| inclination: | 53.1581° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 21.8740° |
| argument of perigee: | 140.0755° |
| revolutions per day: | 15.69879716 |
| mean anomaly at epoch: | 220.0317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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