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 63978U 26145.30050892 +.00000000 +00000-0 +34071-3 0 00009
2 63978 43.0002 100.0258 0001003 268.9425 91.1312 15.27587736 08
| Epoch (UTC): | 25 May 2026 07:12:43 |
| Eccentricity: | 0.0001003 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.0258° |
| argument of perigee: | 268.9425° |
| revolutions per day: | 15.27587736 |
| mean anomaly at epoch: | 91.1312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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