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 62140U 26145.23954557 +.00000000 +00000-0 +54676-3 0 00005
2 62140 43.0017 86.1085 0001558 264.6287 95.4387 15.27597153 03
| Epoch (UTC): | 25 May 2026 05:44:56 |
| Eccentricity: | 0.0001558 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 86.1085° |
| argument of perigee: | 264.6287° |
| revolutions per day: | 15.27597153 |
| mean anomaly at epoch: | 95.4387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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