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 62053U 26145.51606950 +.00000000 +00000-0 +53028-3 0 00000
2 62053 43.0024 189.5085 0001101 246.2571 113.8165 15.27586721 06
| Epoch (UTC): | 25 May 2026 12:23:08 |
| Eccentricity: | 0.0001101 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.5085° |
| argument of perigee: | 246.2571° |
| revolutions per day: | 15.27586721 |
| mean anomaly at epoch: | 113.8165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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