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 62278U 26144.84221551 +.00000000 +00000-0 +13403-2 0 00006
2 62278 43.0009 318.0749 0003092 264.7319 95.3196 15.70925608 07
| Epoch (UTC): | 24 May 2026 20:12:47 |
| Eccentricity: | 0.0003092 |
| inclination: | 43.0009° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 318.0749° |
| argument of perigee: | 264.7319° |
| revolutions per day: | 15.70925608 |
| mean anomaly at epoch: | 95.3196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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