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 62378U 26144.96725727 +.00000000 +00000-0 +28002-3 0 00006
2 62378 44.9877 59.7520 0000709 150.0048 210.0876 15.29341754 04
| Epoch (UTC): | 24 May 2026 23:12:51 |
| Eccentricity: | 0.0000709 |
| inclination: | 44.9877° |
| perigee height: | 477 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 59.7520° |
| argument of perigee: | 150.0048° |
| revolutions per day: | 15.29341754 |
| mean anomaly at epoch: | 210.0876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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